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exd emitted over the forward half space is thus in the form: ext = 2Jtloext = r /D. Given typical values, that is with r ~ 5 mm and D ~ 40 mm, m = Rn,080,o -1 = (I /JJ!) sin =1= 0, a similar, longer calculation results in: III _ L -
I
IOext cos
1/2 space
l
rrp
cos
0
= 2JtlOext 10t'" sin
(21 )
8 Relationships between fluxe s Given that the emitted external flux is a fraction of the total internal emitted flux, and conserving the overall beam power,
z
1
- 2
2n
(22)
VIII Fabrication of optoelectronic components
225
We can obtain the same result directly by the division of eqns (20)/(19) as ie = ext . The factor 1/2n 2 represents the actual yield or 'optical yield' of rays emitted from the LED. d External and internal quantum yields
a External quantum yield The external quantum yield (l1exd is defined as the ratio of the number of protons emitted by a diode (NPhext) in to the external half space over a time t divided by the number of electrons injected (Nel) over the same period of time. Ilext can be expressed therefore in the relationship: Ilext
NPhext t Nphext =-- = -. t
Nel
Net
(23)
If Ie represents the current injected into an electroluminescent structure, we have: Ie = Q/t = Nelq/t, where q is the value of elementary charge (q = 1.6 x 10- 19 C). Thus: Net = Ieq (24) t
For a given wavelength A.d' the energy of the photons is determined by Eph = hC/A.d . With the emitted external flux being ext = Welt (eqn (I) for constant flux over time t), now Nphext
Nphext A.d = -We , that IS. - = -ext. Eph
t
he
(25)
From eqns (24) and (25), eqn (23) for 11ext can be written, for a pseudomonochromatic ray, as qt..d
T '
~ Internal quantum yield The internal quantum yield is defined in the same way as the external quantum yield, with the exception that the number of photons emitted internally in the half space (Nphint) is used:
. _ Nphint t _ Nphint 11lOt - - - - - - - . t Net Nel With Np~inl = ~~
T'
Given eqn (22), on making the division eqns (26)/(27), we directly obtain: I 11ext = 2n2 Ilint -
(28)
226
Optoelectronics of moleculesand polymers
3 Measuring luminance and yields with a photodiode a General notes on photodetectors: sensitivity and spectral sensitivity Typically, a photodetector, or photodiode, gives to a responsive current (Ipho) in a form arising from two origins: •
•
dark current (10) which appears once the photodiode is placed under darkness while polarised in the same way as when exposed to light. This current 10 can arise from two causes. The first is of thermal origin and is associated with the liberation of conducting electrons by thermal excitation, and the second is associated with the generation of charge carriers by ambient beam effects (natural rays); and photoelectric current (lp) associated with the formation of photo-carriers, such as particularly mobile photo-electrons.
ex Sensitivity For a given photodetector subject to a lum inous flux, consisting not necessarily of mono-chromatic light , there is a resulting current: Ipho = 10
+ Ip.
Normally, if conditions remain unchanged during the analysis then the current 10 remains constant, however, I p will change proportionally with the received flux (cf>e), as long as the photodetectors acts linearly. So: Ipho = 10
+ crcf>e
And this expression is only valid for fluxes which are such that cf>e < cf>s, cf>s being the level above which the photodetector is saturated, as detailed in Figure VIII-22. In general terms, the sensitivity of a photo detector is defined by its characteristic slope shown in the above Figure, i.e. c = ~I:: . For a non-linear photodetector, the value is dependent on the incident flux. However, for a linear photodetector, cr is a constant, up to cf>e = cf>s, and takes on the form : (29)
slope o
10
o
ll>s
Figure VIII-22. Linear photodiodecharacteristics.
VIII Fabrication of optoelectronic components
227
~
Spectral sensitivity The spectral sensitivity, for a particular ray of light of wavelength A, is defined by the relationship (30)
For a photodetector exposed to a monochromatic beam of a given wavelength Ad and flux e(Ad), the total number of photons received by the detector per second (np) is np = Ad
= l]Tnp = l]T
Ad e(Ad) hc
= G(Ad).
This coefficient, just like the intensity Ipho of the resulting current, is dependent on the wavelength of the incident light. For a linear detector, the component Ip of Ipho is in the form Ip = FqG where F is a factor of amplification. On taking into account
we arrive at
which can also be written cr(Ad) = Ip(Ad) . e(Ad)
(30')
If the light is polychromatic, the current lp is therefore such that :
Ip =
f
dIph (~)
f
cr(}')de(}.)
f
= cr(A)~(A)dA =
f I~(}')d}'.
(31)
We thus have:
r,
-e -
f cr(}')~(}')d}' e
(4)
-
f cr(}')S(}')d}' f S(A)dA
-cr . - av-
(31')
and the value cr av then obtained for the ratio Ip/e appears as an effective (average) sensitivity. Furthermore, eqn (31') also gives: _ I ---;;-,,-f_S(_A_)d_A_ e - pf cr(}')S(A)dA . With eqn (4) we reach: ' ().) _ I SeA) e - P f cr(A)S(A)dA .
(32)
228
Optoelectronics of molecules and polymers
In addition, eqn (30) gives ~ (A) = I~(A)/a(A), which leads, by comparison with the previous eqn, to , a(A)S(A) (32') Ip(A) = Ip a(A)S(A) dA
J
.
b Example photodiode set-up [Ant 98] Photometric measurements are typically performed with a photodiode that has as large a surface area as possible, for example of the order of 100 mm 2 . a Example values for a(A) As an example, Table VIII .1 shows values given by Radiospares for a standard diode, with spectral response between 350 and 1150 nm, for a(A) at different given wavelengths A = Ad. ~ Device set-up In order to measure the luminance of OLED components, the photodiode is placed up against a window open to the OLED and is connected to an amplifier. Thus by the action of a resistor (Rc) placed in the circuit detailed in Figure VIII-23, the assembly permits determination of the value of I p from the voltage (Vp = RcIp) indicated by a multi meter. (Technical note : the amplifier typically used for this sort of assembly is powered by a tension (Va) equal to 18 V, while the tension applied at the photodiode (V phol is of the order of 10 V. The potentiometer, tied to an operational amplifier, allows this offset tension to be disregarded. The charge resistance is fixed at 995 ohms).
Y A classic set-up for measuring luminan ce: representation ofn and apparent OLED surface (Sa) In general terms, Sa is the apparent emitting diode surface, and is such that Sa = As cos a (see Figure VIII-19) . Practically speaking, the measurement of a beam emitted by an OLED is effected by placing a photodiode at the window of the measuring cell, as shown above in Figure VIII-24. The surface of the photodiode is perpendicular to the beam direction, so if we designate the surface of the OLED by SD, the apparent surface Sa is such that Sa = SD. Typically, the surface of the photodiode (SPh) is around 1 cm 2 while the surface of the photodiode is more like several mrrr' . In effect, the source acts as a point with respect to the receptor.
Table VIII.I. Principal sensitivity values for a standard photodiode ).,(nm) 400 450 500 550
a( ).,) (A W- 1 )
)., (nm)
a( ).,) (A W- 1 )
0.12 0.2 0.25 0.28
600 650 700 750
0.32 0.35 0.38 0.42
VIII Fabrication of optoelectronic components
229
Photodiode
-Vpbo
FigureVIII-23.Amplified photodiode set-up .
The half angle at the apex (
Source (So)
Photodiodc (sp/»
FigureVIII-24. Simplified scheme of diode/photodiode arrangement.
230 Optoelectronics of molecules andpolymers
c LED luminance determination using the present example of an OLED a A mono- or pseudo-monochromatic LED (A = Ad) In practical terms, if Ip = Ip(Ad) is the current generated by a photodiode under a beam of light emitted by an LED at a solid angle Qph, then given eqn (30') , e(Ad) is the flux ph ' and we can write: <J(Ad) = Ip/ph. Ip is such that Vp = RcIp (see preceding Section ~). From eqn (12), (33)
Introducing eqn (33) directly into eqn (15) directly gives: Km V(Ad)V p . RcQphSO<J(Ad)
Ly =
(33')
We can also write (34) It is eqn (34) which is widely applied, even to polychromatic sources, however, as we shall see in such cases, the factor D should be replaced by a factor called 'A' which will be defined below. Clearly, the ratio A/D will indicate the extent to which the approximation of a polychromatic to a monochromatic source remains correct. ~ Polychromatic source
Following eqn (30), we have <J(A) = I~(A) /~(A) ; from eqn (12) we can write, L~ =
Qp~SD ~~i
'we can go on to substitute the value ofI~('A.) given by eqn (32'), ,
Ip SeA) 00 QphSo f o <J(A)S(A)
Le = -
ax
(35)
•
On transferring the value of Ip = Vp/R c in to eqn (35), we obtain
L~ (A)
=
Vp RcQphSO
00
SeA)
fo <J(A)S (A) . ax
.
(36)
The desired expression is finally obtained by introducing eqn (36) into eqn (16): VpKm fV(A)S(A)dA t, = RcQphSO f <J('A.)S(A) dA'
(37)
which can also be written as VpKm t,
.
= ARcQphSO' with A =
f V('A.)S('A.) d'A. f <J(A)S(A) dA =
Vay <Jay ·
(38)
(<Jay is defined by <Jay = f <J(A)S(A) dA/ f SeA) dA and Vay in a same way by Vay = f V(A)S(A) dA/ f SeA) dA).
VIII Fabrication of optoelectronic components
231
Table VIII.2. Comparison of A and D terms for green and blue diodes.
Diode Green (532 nm) Blue (467 nm)
A (lm A- 1) 1485 698
2224 256
0.67 2.92
y Numerical application [TroOJ} By way of example, and for two differentOLEOs, Table VIII.2lists values for 0 (pseudo-monochromatic) and A (polychromatic) terms. The latter is calculated by numerical integration of empirical values obtained over the electroluminescent spectrum. One of the OLEOs emits light centred on the green light (Ad = 532 nm), while the other is centred on blue light (around Ad = 467 nm). We can see that the coefficients A and 0 are neither equal nor proportional. The use of the pseudo-monochromaticapproximation results in: • •
overestimation of polychromatic luminancefor an OLEO which emits in the green region as OOLEDgreen > AOLEDgreen; and underestimation of polychromatic luminance for an OLEO which emits in the blue region as OOLEDblue < AOLEDblue.
We can thus see the interest in determining luminance through a polychromatic 'configuration' which does not penalise blue OLEOs, that in principle exhibits lower luminances than green OLEOs. It is worth noting though that the precision available for polychromatic observations is tied to that of the experiment used to determine the electroluminescent spectrum. d Characterising yields
a External yield The external yield is given by eqn (26), that is Ilext = h~d CI .
laser systemwith constant opening
Figure VIII·2S. Schematisation of the equipment used to measure losses due to propagation.
232
Optoelectronics of molecules and polymers
intensity given by eqn (7), which represents the flux within a solid angle unit, here
=
In addition, lext IOext cos lp, and with I Ip F' 11 '" _ I - 1l Qph a(I..)· ma y, 'i-'ext - Jt Oext - Q ph
=
lp ~
=
=
7° and cos lp 0.992 ~ 1, lext IOex d '" - 1l Vp Placi a(l..) , an 'i-'ext - Qph Rca(I..)· acmg thiIS into Ip
eqn (26) yields:
Vp he QphRe a()..) t, q
Jt
)..
Ilext = - - - - - - .
(39)
~ Internal yield According to eqn (28) , we have llint = 2n211ext. which allows us to write (40)
IV Characterisation of polymer based linear wave guides [Col 98 and Ebe 93] The titled characterisation is generally performed using wavelengths used in telecommunications, that is 1.3 and 1.55 11mand allows analyses of: • • •
light transversally diffused by the guide; losses due to propagation, injection and diffusion at the extreme surfaces; and the transversal profile of the beam issued from the guide.
1 Measuring transversally diffused light Figure VIII-23 schematises the equipment used to specifically mea sure losse s due to propagation within the guide, a loss especially important when using polymer based materials. The source used in the system is a fibre based laser diode, which emits a transversally sinusoidal beam. A collimator, placed at the exit of the fibre, gives rise to a plan limited wave with a divergence minimised by diffraction. A 20x multiplying lens 'injects' the wave into the guide (G) and the position of the lens and the guide are optimised with the aid of micro-positioning elements. Light diffused by the guide
· x'
guide
z -=========~=========-. . z' x Figure VIII·26. Configuration for analysis of transversal.
VIII Fabrication of optoelectronic components
233
o Guide
- --I••
P
Figure VIII-27. Configuration used to measure losses by 'cut-back' .
and perpendicular to propagation direction zz' is analysed using a camera equipped with a vidicon tube (sensitive in the range 400 to 1800 nm). The video signal, resulting from a sweep parallel to xx' is digitised and treated with a computer program (Figure VIIl-26) .
2 Loss analyses using 'Cut - Back' and 'Endface Coupling' methods a 'Cut - Back' Initially, a collimated laser wave is injected into the guide using a 20 x lens and global losses are determined by observing the difference in power between the injected (Pe) and exit (Ps) light, as detailed in Figure VIIl-27. Following the simple principle method of 'cut- back' , measurements are repeated using different lengths of guide (z.), yielding a curve shown in the upper part of Figure VIII-29 with a slope due to propagation losses .
b 'Endface Coupling' [Ebe 93] The method of 'endface coupling' uses the set-up shown in Figure VIIl-28 and allows differentiation of losses due to injection from other losses . A light beam traverses the guide from edge I to edge 2 initially in order to select the modal profile exactly adapted to the guide . An autocollimator made from a lOx lens and a mirror M injects across
guide
lOX
M 'c hopper'
.-
Figure VIII-28. Layout for 'endface coupling ' equipment.
234
Optoelectronics of molecules and polymers
dB Cut- Back :
10
Lea= Lp z + Lc with
Slope: losses by propagation
OEC :
(L~
..-5-
······································X· ··············
.
--------------------1--------------------------._.J~~._._._. "_,_,_,,_,_,_,,_,_,,_,_,, nappropriate modes
LMM
FRESNEL
LoEC = Lp Z + L~
with
L~ =LFR + Ld
Diffusion (edge) Ld
o
z (guide length)
Figure VIII-29. Curves permitting analysis of different optical losses (see text for definition of parameters).
side 2 the initially filtered mode without any losses due to interference. With several guide lengths, we can obtain the curve denoted by letters OEC in Figure VIII-29 .
c Curves representing optical losses Figure VIII-29 shows various curves which allow analysis of the relative weight of different losses : • • • •
• •
LCB losses measured by 'Cut - Back'; LOEC losses measured by 'Optimum Endface Coupling' ; Lp losses due to propagation; LpR losses due to FRESNAL (reflection) ; Ld losses due to diffusion at terminal edges; and LMM losses by injection due to imperfect covering of injected and modal profiles.
IX Organic structures and materials in optoelectronic emitters: applications and display technologies
I Introduction During the last half of the 20th century there has been an extraordinary development in communication and information technologies. The dominant tool used for visualisation in televisions, computers, radar screens, medical imaging, to give j ust a few examples, has been the cathode ray tube (CRT). Recent requirements, for portable computers, phones, watches and so on, which require lightweight , unwieldy screens operating at low voltages, have also vitalised the development of new electrical component s such as light emitting diodes (LEDs) and, less recently, screens based on liquid crystals. Given the rapid pace of development in display technologies and its results (micro-point plasma screens, electroluminescen t screens based on inorganic and subsequently organic materials) it is now possible to imagi ne performances which were previously inconceivable in devices such as wide-screen (greater than 35/1 ) high definition televisions, light ultra-thin screens which could be easy to move or store, and flexible screens permitting ergonomic designs in cars and civil and military aircraft (dashboards, screens in helmets for weapons sighting and so on). In this Chapter, we have chosen to present the main types of display systems, and then to compare organic component technology against that of classic components. We shall also rapidly detail the process of converting an incomin g electrical signal into visual inform ation in optoelectronic components. This process is typicall y due to luminescence (luminous emissions not entirely thermal ) which can be provoked via various route s, such as photonic excitation (generally in the ultraviolet), excitation caused by excited particl es (cathodic lumin escenc e due to electrons), and application of an electrical field (electroluminesce nce) to give the principal examples [cur 56].
II How CRTs work CRTs operate on the principle of cathodoluminescence. This is due to the impac t of a beam of accelerated electrons on a surface dotted with ' phosphors' points, or contacts, which on relaxation to an equilibrium state following excitation, emit light in the
236
Optoelectronics of molecules and polymers
Figure IX-I. Arrangement of 'phosphorus' blue (b), green (g) and red (r) contacts on a cathode screen.
visible region . Sections VII-I and VII-2 detail the process of electroluminescence in inorganic materials and, in particular, these 'phosphor' contacts. Luminous emissions from colour televisions are seen by the human eye in an additive process, in a manner similar to that observed through impressionist paintings which are based on the juxtaposition of coloured points (pointillism) [Til 00]. Each luminous element, called a pixel (from the contraction of 'picture element'), is in fact the product of three 'sub-pixels' (contacts placed as shown in Figure IX-I) each generating one of the three primary colours (blue, green and red). Each contact is composed differently to give the different colours: activated silver with zinc sulfide (Ag: ZnS) for blue, activated copper and zinc and cadmium sulfide (Cu:(Zn,Cd)S) for green, and activated europium and yttrium oxysulfide (Eu3+ : YzOzS ) for red.
III Electroluminescent inorganic diodes Electroluminescent inorganic diode s underwent expan sion in use towards the end of the I960s due to their lost cost (per industrially produced unit), their long lifetimes, their ability to emit light over a wide spectral range and their ease of control by a simple electronic circuit. They are widely used in domains requiring small emitters (digital displays for measuring devices and some calculators) and as calibration standards. While their individual price is low, the large number required to make an high definition screen from them makes such an overall cost prohibitive, adding incentive to finding alternative display technologies.
1 How they work In relatively simple terms, an LED is made from a directly polarised pn junction. Under the effect of this polarisation (V), charge carriers are injected from one region , where they are in the majority, to the other, where they are a minority. So electrons from the n side are injected into the p side, while holes are injected from the p side into the n side. Figure IX-2 shows this crosso ver. During the diffusion of the charge carriers, which for electrons is of length Ln and for holes is of length Lp, the minority carriers can recombine with majority carriers (minority electrons with majority holes in zone p and minority holes with majority
IX Organicstructures and materials in optoelectronic emitters 237 Zonep
Zonen
••••••••
Figure IX·2. Radiative recombination zones in a light emitting pn junction working under direct polarisation.
electrons in zone n). Usually we neglect the number of recombinations in the zone ZCE (Figure lX-2) which tends to be particularly narrow under typical tensions (V) [mat 96] . If the semi-conductor used is at direct gap (that is with the minimum conduction band and maximum valence band, in reciprocal space , at the same wavevector value), then electron-hole recombinations are facile as a third assisting particle is not required (such as a phonon for which the wavevector assures the conservation of the quantity of movement for indirect transitions-which are oblique and characteristic of semiconductors with an indirect gap such as silicon). The emission of photons corresponding to this recombination occurs with energy of the order of the size of the band gap. For GaAs (direct gap) this is equal to 1.43 eV, an emission with a wavelength ('A.) of 0.861J,m and in the near infrared.
2 Display applications To use semiconductors in displays requires the use of GaP which exhibits an indirect band gap of around 2.3 eY. Due to this indirect gap (and to reinforce radiative recombinations) impurities such as nitrogen are introduced into the semiconductor to form donor type states close to the conduction band [bre 99] . Excitonic radiative emissions can thus be generated in the green region of the visible spectrum with GaP(N) . Other colours can also be obtained, for example by doping GaP with zinc or oxygen, or by using mixtures of semiconductors such as GaAsl-xPx . In the latter case, the direct gap in GaAs increases with the concentration of phosphorus. With a direct transition, a red emission can be obtained using 40 % phosphorus, while orange and yellow emissions occur on adding nitrogen to varying compositions of GaAsl -xPx. Finally, blue emissions can be obtained using GaN or with the alloy InGaN .
3 Characteristic parameters (see also Chapters VIII and X for further definitions) The internal quantum yield, which is defined as the ratio of photons produced to the number of injected electrons, can reach 50 % in direct gap semiconductors. However, the external energetic yield (ll) which represents the ratio of luminous energy to the
238
Optoelectronics of moleculesand polymers
10 cosS
Figure IX-3. Lambert's emission represented. electrical energy supplied is typically of the order of I to 10 %. The mechanisms which result in this difference can be classed into three types : •
•
•
the absorption of photons by the material which they traverse (for which multi layer structures of materials with gaps above the emissions energy have been designed, so as to limit such absorptions); Fresnel losses which result from a difference in the refraction indices of the diode and air giving rise to the reflection of a part of the wave and its associated power; and losses due to total internal reflection when photons emitted strike the diode/air interface at an angle greater than the limiting angle (indice of diode is greater than indice of air) and remain trapped within the diode.
e,
As detailed in Chapter VIII , the luminous intensity varies according to Lambert's angular law (Figure IX-3), that is I(e) = 10 cos e in which 10 is the intensity in the direction normal to the surface and is the emission angle (again st the normal) . Therefore, if increases, cos decreases along with the luminous inten sity emitted in the same direction.
e
e
e
4 In practical terms Electrons exhibit a higher mobility than holes , and the level of electrons injected into zone p is greater than the number of holes in zone n. The result is that zone p is the principal centre for radiative emis sion s and is thus used as the emitting face of the diode (Figure IX-4) .
n SUBSTRATE
Figure IX-4. Structure of a typical LED.
IX Organic structures and material s in optoelectronic emitters ,, .:
"
I
'
239
Strong incidence ", 0 os 0,) \
! I I
! Weak incidence (0« 0 ,)
Figure IX-S. The role of the posit ion of the dome .
Finally, practically speaking, LEDs are encapsulated with a transparent resin dome which serves three functions : • • •
protection of the diode and its connectors from the exterior; reduction in the difference in indices of the diode and air, thus increasing the overall yield of the diode (reduction in Fresnel losses); and reduction of total internal reflection effects by generating an incidence angle at the dome lower than the limiting angle 81 (see Figure IX-5).
It is notable that for LEDs placed at the summit of the encapsulation dome (the continuous line in Figure IX-5), the largest part of emitted light hits the surface at an angle below the limiting angle. A diode of this type generates a greater angle of view (when looking at the diode) than a diode which has the emitting centre towards the rear of the dome, which emits light that falls on the sides of the dome with an angle close to or greater than the limiting angle.
IV Screens based on liquid crystals 1 General points Liquid crystals (LC)s were developed near the beginning of the 1960s for flat screens and, given the investment made at that time by industry (for example by Thomson LCD), this system remains the most widely used in technologies such as watches, calculators, computer screens and portable telephones. World wide, the market for LC based screens is valued at around 30 billion dollars, just below that of cathode ray tubes. The liquid crystal state is a mesophase, a state in between those of a crystalline solid and an amorphous liquid [Til 00]. There are three main types of mesophase: • • •
Timmerman's globular molecule s which give rise to plastic crystals ; discotic, resulting from flat molecules ; and calamatic, resulting from long molecule s which can be in piled layers (smectic LCs) or grouped in clusters (nematic LCs) in which the molecules are aligned parallel to one another (depending on thermal effects) .
240 Optoelectronics of molecules and polymers
2 How liquid crystal displays work Liquid crystal displays (LCD)s operate by using two basic properties of LCs: • •
the molecules can modify the direction of polarisation of an incident wave of light; and the molecules can be easily moved by the application of an external electrical field, which interacts with an orientated assembly of molecules and their orientated dipole moments (unlike thermal agitation which randomly moves individual dipoles). Even weak fields can vary by a considerable degree the orientation of the molecules. In practical terms, there are two main types of system: [Car 84]
a 'Guest-host' type displays These displays use dichroic dyes (denoted 'guests' ) orientated by the crystal liquid molecules (the 'hosts') . The elongated dye molecules absorb the component light vector parallel to the molecules' axes (see Figure IX-6) but not the perpendicular components (due to dichroism) . Depending on the direction of the molecules , determined by an applied electric field, an incident wave polarised parallel to the molecules (which have an initially homogeneous arrangement) would be reduced or become non-existent. It is in this manner that displays can be prepared using nematic LCs with dichroic dyes introduced into sandwiched cells, constituted of glass plates, 5 to 200 urn apart, covered with the transparent conductor ITO (a mixture of indium and tin oxides). In reality, two optoelectronic effects may be observed: the first corresponds to an inversion of contrast (from an initial homogeneous orientation as in Figure IX-7-a) and the second a normal contrast (from an initial homotropic orientation as shown in Figure IX-7-b).
b Displays made with helical nematic liquid crystals These are the most widely used and are based on the rotation of the plane of polarisation of light by 90 0 by 'twisted' nematic liquid crystals, in a configuration shown in Figure IX-8.
wave Figure IX-6. Usinga dye to modify wave polarisation.
IX Organic structures and materials in optoelectro nic emitters
Incident light
lncideut Iiaht
( )
Polarising filter a ;5 GIll! cover
•
I
Glass cove r
- : .- : .
-=-
Dye
illP l ~
Polari sing filter axis
I
~
Layer of ITO Liquid CI"),tltl/
24 1
_
1..a\'erofITO
Uq";d'~ ~I./" D )' c
r = = = = = =1' ••
I
I
_
I
.....
Light cut off
I •
Light tran:millcd
Incident light
Incident light
(b)
Polari sing filter axis Glu ' cover
I
I yer of ITO
Liquid Cf)"tHI/
Dye
Polartslng fllter axis GIll! cover I
•
I I I
I
~
~
I
.
I
. ..
••
• I
~
Layer of ITO Liquid cr)"lal/
_
- : .- : .
L-
~I
~
Dye
•
Light cut off
I rausruitted light Figure IX-7. (a) Initially homogeneous orientation: inverted con trast; and (b) Initially homotropic orientation: normal contrast.
The liquid crystal is encapsulated between two glass sheets around 10 u.m apart each covered by a transparent ITO electrode, The glass sheets are surface treated so that on contact with the liquid crystal, the molecule s of the latter align themselves along a given direction . In addit ion, the directions of molecules at the two electrodes are such that there is 90° between them. As shown in Figure IX-8-a, a polarising filter, on the upper side, allows only incident light orientated parallel to the LC molecules through. Throughout the thickness of the LC layer, the molecules turn this single light component so that on reaching the lower face, the light is polarised parallel to the seco nd polarising filter. Thus, in this relaxed state, the system appears transparent. Once a tension is applied, using the electrodes detailed in Figure IX-8-b, the electric field orientates the LC molecules so that they are parallel to the propagation component of the incident light. The LC molecules no longer turn the direction of the polarised traversing light and therefore, when the light reaches the lower face, it arrives with a component perpendicular to the second filter and the system now appears opaque.
242
Optoelectronics of molecules and polymers
Polarising filler
layer used to align LC
molecules
LC molecules
layer used 10 align molecu les
L~~~""I lII!l
Polarising filter Light transmiued: 'clear" . n...,n
~
Opaque system: black screen
Figure IX-8. (a) Without polarisat ion oflight in between electrodes , LC are in helical form and system allows light to pass : observer sees transparent system; (b) With electric field applied (~l V), the initial orientation of molecules is disturbed and light is no longer turned to pass through the second polarising filter: the observer sees an opaque system .
The response time of such a system can be of the order of several tens of milliseconds, a value which permits the use of these materials for display technologies (which rely upon the persistence of perception of light of the human eye).
3 LCD screen structure and the role of polymers Screens are made up of a matrix of rows and columns of pixels (to give a matrix screen) . Colours are obtained by dividing each pixel into three sub-pixels (red, green and blue), each of which can be individually addressed. A side view is given in Figure IX-9.
DilTuser Polarising filter 3 comma nding electrodes Commanding column_~t;J."'-=~I!IIt:;lI!l!l. Comma nding row Liquid crystal Common electrode Layer of coloured filten>--fL-Polarising filter Glass substrate Figure IX-9. Cross section of a LCD pixel.
IX Organic structures and materials in optoelectronic emitters
243
Polymers are involved at several levels in the manufacture of LCD screens and help in reducing their energy consumption and facilitating their use, by introducing qualities such as low weights, flexibility and so on [bro 01]. They are used in particular in the following ways : • • •
•
photosensitive polymeric resins used in the photolithographic processes; in cons tructing the screen and the walls of each cellu lar pixel which contains active materials ; in aligning and orientating layers ofliquid crys tals, with the recent use of polymers that have improved the viewing angle and have allowed , using a stamped film layer of polyimide, control over the alignment of molec ules in each sub-pixel; and optical functionalisation of screens, whereby stretched polyvinyl based polarising filters are protected by cellu lose triacetate, which are filters coloured by photosensitive acrylates. Diffusion of light can be obtained using a stretched polyester film. Indeed, mixtures of birefringent polymers can be used to generate reflections by diffusion of otherwise untransmitted, polarised light permitting a recovery of this unused light. Using these techniques has allowed an increase in the luminance of screens, from around 200 cd m- 2 for the more classical systems based on backlighting to around 500 cd m- 2 , a value similar to that obtained with cathode ray tubes.
4 Addressi ng in LCD displays [Dep 93] Multiplex addressing (reaching any single pixel at a given moment) necessitates a system for addressing each pixel in a display[bar 00] . In passive matrixes , as shown in Figure IX-1O-a,each pixel is addressed via the use of a system of electrodes placed in rows, placed for example on the upper glass plate, and in columns, placed for
(a)
Impulsc tensions applied at columns
u unnuuu .-
R~
impulse tcjlot
-
-
-
-
-
.-
I I I I I I Selected ells
Fig ure IX-l O. (a) Passive matrix addressing; and (b) Active matrix addressing.
244 Optoelectronics of molecules and polymers example on the lower glass plate. At each intersection is a pixel. The surface of the screen is swept in a 60th of second by the electrical excitation of each row while each column is subject to a tension sufficient to produce the required excitation of each pixel. Pixels which are not selected for illumination are subject only to a low or residual tension, the latter of which increases as the resolution of the screen is increased . Indeed, to increase the resolution, along with the number of rows, the tension needs to be increased to maintain an overall average luminance of the order of 200 or 300 cd m- 2 ; any increase in resolution also necessitates a decrease in contrast as otherwise some pixels would be illuminated simply by going over the threshold tension . In order to resolve the problem of decreasing contrast with increasing resolution, active matrixes are used which have individual command transistors associated with each pixel. These transistors are called thin film transistors (TFf) and consist of two electrodes for the entrance and exit of current which flows under the control of a third gate electrode . Hydrogenated amorphous or polycrystalline silicon has been widely used although electroactive polymers have been used as organic electronic / optoelectronic materials . Examples of polymers developed for such use are poly(para-phenylene vinylene) (PPV) [gre 95] and polythiophene, and such materials being more and more widely used. A more detailed description of the function of organic transistors can be found elsewhere [hor 00].
5 Conclusion In conclusion, the technology used for LCDs is now very wide spread and has given rise to screens which operate at low power rates. One of the major limits of the technology, however, is the viewable angle of LCD displays , at around 30 0 to 40 0 , which results from the technology itself (molecular alignment forming a directional guide), although some progress has been made in improving this [jon 99]. Hitachi and NEC have realised displays with excellent viewing angles by using coplanar electrodes which control, in the same plane, the optical commutation of the liquid crystals. In addition, very wide screen displays, for example for use as wall televisions, have been prepared (from 1990 on by Tektrononix) by replacing the TFTs by plasma canals which successively trigger each row of pixels.
V Plasma screens Plasma screens were developed around the beginning of the 1970s following the demand in flat screens. Monochromic plasma screens operate by emitting orangeyred light from ionised gas, much in the same way as neon tubes[dep 93]. The gas, confined within a series of small cavities each positioned at the intersection of upper and lower electrodes (which determined the size of the pixels, as shown in Figure IX-II), is excited to the plasma state by applying a certain, selective tension. Displays made using this technology exhibit high brilliance and good lifetimes and stabilities. However, they require a considerable amount of energy to operate (and run
IX Organicstructuresand materialsin optoelectronic emitters
245
Insulator-i~:;::=~~~ Upperelectrode-s Magnesium oxide Pixel or sub-pixc eparator Neon + xenon Phosphor -t:::::~~-==t=l Lowerelectrode Glas
Figure IX-H. Cross section of a plasma screen.
at around 200V). Other colours can be made by indirect excitation of luminescent substances (again using primary colours) with a plasma that emits in the ultra-violet, an example of which is a gaseous mixture of neon and xenon . The geometry of each sub-pixel, which emits either red, green or blue , is shown in Figure IX-II. The cavity, containing the excitable gas is covered with one of three phosphors. The layer of magnesium oxide is there as a dielectric to reinforce the electric field within the cavity [Til 00].
VI Micro-point screens (field emission displays (FED)) FEDs are microelectronic components which approximate to miniature cathode ray tubes [Bre 99]. In a FED, electrons are emitted from a cathode and collide with a phosphor to give an excitation and thus a luminous emission. Cathodes are assembled above an insulating layer, as shown in Figure IX-12 . Each pixel contains three phosphors and three metallic electrodes which play the role of gates for each colour.
anode
gate electrode
gate electrode
Figure IX-12. Cross sectional structure of a micro-point screen (FED).
246 Optoelectronics of molecules and polymers A pixel is activated firstly by the application of a threshold tension (cathodic tension). Any current that flows is controlled with the help of a variable tension applied via the gate electrode. This controlled current of electrons is then accelerated towards the anode . The primary electronic current, which has a more or less radial propagation, is then focussed by use of gate electrodes placed about the micro-point cathode so that the electrons reach the anode in a nearly parallel beam. FED based screens exhibit several advantages over cathode ray tubes and vacuum tubes: • •
they can produce a higher current density during thermo-ionic emission than that encountered in vacuum tubes ; and they do not require filament heating as electrons are generated by a field effect obtained at the extremity of a micro-point cathode, where the field is sufficiently intense to develop electrons through tunnelling effects across a reduced, narrow potential barrier between micro-point tip and the vacuum (see also Annex A-7, Section III).
With respect to LEDs based on semi-conductors, FEDs also present some advantages: • • •
no losses due to dissipation ( i.e. no colli sions between electrons in the vacuum while electrons may collide with a semi-conductor lattice); operation practically independent of temperature; and no perturbations due to ionising rays.
However, FED based screen s do pose some disadvantages, for example the minimum distance required between anode and cathode to reduced sparking, and the non-directed emission of electrons tending to limit the obtainable degree of resolution.
VII Electroluminescent screens 1 General mechanism Electroluminescent screens function using Destriau's effect [mat 96], in which radiative recombinations are generated by the application of an electric field to a powdered semiconductor dispersed within a dielectric matrix, as shown in Figure IX-13-a . The semiconductor is normally the mixture of an inorganic material from group s II-VI, with a relatively large forbidden band of around 2 to 3 eV, and an activator made of a transition metal (typically copper of manganese) or a rare earth . In addition, fillers such as NaCI or KCI may be used as they are easily melted and on cooling they favour the formation of crystals and the insertion of the activators . The electric field plays the role of carrying the concentration of free charge carriers above its equilibrium value; a return to equilibrium results in recombinations and, in the case of radiative recombinations, the emission of photons. The concentrations, outside of equilibrium, can be generated (and can accumulate) by applying a strong enough field. In general :
IX Organic structures and materials in optoelectronic emitters
(b)
;1
Sn02
Dielectric
/V
ZnS
u
(a)
ZnS -
247
·C /
....o
~
o
Q
lctallic electrode
BV
E applied
Figure IX-13. (a) Structure assisting the Destriau effect; (b) Mechanism of charge injection into electroluminescent (ZnS[Cu]).
•
•
when E, < 108Ym- l , shock ionisation proce sses (with Wionisation = q E, I, where I is the distance covered by an accelerated carrier between two impacts) shift electrons into the conduction band of the semiconductor from valence or impurity bands ; or when E, > 108 Y m -I , carriers can be injected through tunnelling effects at the interfaces (see Figure IX-I3-b) to increase the density of carriers available through shock ionisation.
The component structure of electroluminescence will vary depending on the type of applied tension (altern ating or direct).
2 Available transitions in an inorganic phosphor In the band scheme of an inorganic phosphor there are permitted bands associated with activators (otherwise called luminescent centres when they induce radiative transitions). There are two possible types of centre within a phosphor: •
•
those which introduce into the forbidden band localised levels close to the valence band ; this is the 'classic' model of Cu centres in ZnS which give rise to a level at several tens of eV above the valence band that has a high probability of capturing holes ; and those which reinforce both the fundamental level I close to the valence band and the excited level II just below the conduction band. Levels I and level II exhibit high probabilities of capturing holes and electrons, respectively. An example of such an activator is CuCI, [dep 93] although Mn3+ is more widely used along with rare earth ions [mom 95] .
There are other bands, very clo se to the conduction band , which also exist. They are associated with structural defaults (and thus the preparation of the phosphor) and act as trap levels . Electrons caught with in these bands may be thermally released with a probability given by the Randall-Wilkins law, which supposes that electrons within the traps have a Maxwell type distribution of thermal energies (see also Chapter VI,
248
Optoelectronics of molecules and polymers
Section IV-4). It can be written in the form p
= Vo exp( -Us/kT),
where Us is the energetic depth of the trap with respect to the edge of the conduction band and vo,a priori, is a constant which takes on a value of the order of the frequency ofphonons (;::::;10 12 sec-I according to Mott and Gurney) although it does tend to vary with temperature and typically has been found to have a value around 108 sec"! in phosphors [ran 45]. Figure IX-14 shows a representative energy diagram for activated phosphors [fri 85]. There are various transitions which can be envisaged: • • • •
•
A: an activator is excited, recombination occurs and an electron returns to the fundamental level; B: excitation, in the conduction band, of an electron at an activator and a recombination with another activator centre; C: same as B but with a delayed recombination due to the passage of electrons via trap levels, which they escape through thermal energy; D: band to band generation due to energetic beams (>2 to 3 eV) whereby a free hole generated from the valence band is displaced until it recombines with an electron in the neighbourhood of an activator. The latter acts as a radiative centre, and an activator electron falling from the valence band to recombine with a hole results in a positive ion at the activator itself, which may in tum may capture, radiatively, an electron from the conduction band; and E: the same process as D but a similar delay to that in process C in which electrons are delayed by traps .
Generally speaking, the term 'fluorescence' is used for immediate relaxations (for example, cutting out trap levels and within a time 1: ;::::; 10- 8 s) while the term 'phosphorescence' is used for recombinations which occur after a delay 1: > 10-7 s. Comment It is worth noting that while an increase in temperature may help detrapping of electrons , it can also lead to an extinction of luminescence. This is due to electrons excited from the valence band to empty levels of the activation centres,
Conduction band Traps Activators' excited levels
u
E~:::':-='::~:::'
.:- ::::::.~::: '~:::-:'': ::~ ..::.:~~:: ::::: :: ::~:::.:: BCD
Act ivators' fundamental level
E
_ ._. ._. _. Valence ham!
....._---------~----
Figure IX-14. Energy levels in a semiconductor (II-VI) activated by transition metals or rare earths.
IX Organic structures and materials in optoelectronic emitters
249
Table IX .t A. (nm)
ZnS (blende) ZnS (wurtzite) CdS (wurtzite) ZnSe (blende) CdSe (wurtzite) ZnTe (blende) CdTe (wurtzite)
341 335 510 477 711.5 578 871
E (eV) 3.64 3.70 2.43 2.60 1.74 2.15 1.42
which can therefore no longer act as recombination centres, or excitation of carriers simply to be trapped non-radiatively at extinction centres.
3 Characteristics of inorganic phosphors from groups II-VI [cur 60] Groups II-VI have a forbidden band of energy EG which is close to that of photons in the visible range . The materials most widely used are ZnS (which as zinc blende in Europe or sphalerite in the USA is of a cubic structure, or as wurtzite is of a hexagonal structure) and CdS. Table IX.I below gives the values of EG and the wavelength of corresponding photons for the principal mixtures used. The emission band to band transitions observed for these phosphors actually appear unrealistic, however, it is the introduction ofluminescent centres , as mentioned above typically based on copper or manganese, which permit a circumnavigation of the problem. In Figure IX-IS there is shown the relative position of energy levels associated with copper luminescent centres introduced either into ZnS or CdS . In both cases there are two principal emission bands. In the case of ZnS(Cu) there is one in the green at 527 nm and one in the blue at 445 nm. In classical terms, photoluminescence occurs when centre excitation (by UV light) results in the generation of valence band holes, into which there is then a fall of electrons from luminescent centres (see Figure IX-16-a).
(a)
..
ZnS CB
I
3.70 cV 12.37 cV 2.79 cV I 15Z.\ nm ! (.usom! Cui _t'---_ _ Cull ......:..._-
VB
3cV
VB Figure IX-IS. Energy levels in: (a) ZnS(Cu) ; and (b) CdS(Cu) .
250
Optoelectronics of molecules and polymers
(a) I, citation
t ','IlUl:
electron . CB
• o
o
VB ..,.- - - -Hole
(b) Radiative emission .1uo!J'S'
Pho
•
•
CB
[T o
_....:. 0_ _
VB
Figure IX-16. (a) centre excitation; and (b) radiative emission,
Radiative emission though corresponds to the recombination of conduction band electrons (from group II-VI elements) with holes localised at luminous centres (through process D indicated in Figure IX-14) . If the transition occurs directly, without passing via traps situated just below the valence band, then the emission occurs as fluorescence, however, if electrons relax on passing through trap levels, then the emission occurs as phosphorescence, as shown in Figure IX-16-b. Phosphors based on ZnS are not easy dope so that they are of n or p type, [page 79 of mom 95] and this sort of material cannot be used in a pn type LED.
4 Electroluminescent think film displays: how they work with alternating current A general abbreviation often used in this area is ACTFEL standing for 'A.C. supplies in a Thin Flim Electroluminescent displays' [bre 99]. Typically, thin film electroluminescent displays are based on an insulatorsemiconductor-insulator structure, as detailed in Figure IX-17-a .
D~elecltl c
layer Tunn elling effect injects electrons into CB
------I
ZnS(Cu)
I
(a)
Applied electric field
Figure IX-!7. (a) The different layers in an ACTFEL screen; (b) Band positioning on application of an intense electric field.
IX Organic structures and materials in optoelectronic emitters
251
The active ' phosphor ' layer (ZnS(Cu)), which is about 700 nm thick, is set between two transparent dielectric layers, them selves each about 400 nm thick.The latter layers are in cont act with electrodes , one aluminium, the other transparen t ITO deposited on a glass substrate. Thi s structure resembles that of capacitors in series, and permits the generation of a relatively high tension at the active ZnS(Cu) layer from a low tension at the electrodes by using the low capacities of the thin dielectric layers. On application of a strong electric field (E a ) the high degree of band 'b endin g' of the active layer allows electrons, which would otherwise be trapp ed at interface states, to pass throu gh to the conduction band by tunnellin g effects (Figure IX-17-b). Electron s cross the active layer by collecting energy along their pathway of distance I. With W = e E, I, and starting at the threshold energy, these electrons can transfer by collision a high enough amount of energy to excite the luminescent centres with a return to equilibrium throu gh lumin ous radiation. Given that the concentration of centres is rather low, of the order of lO IS cm- 3 , and that of the phosphor hosts is of the order of 1023 em - 3, the actual available surface for generating impact excitations is very low. Accordingly, only a small proportion of the injected electrons result in the excitation of a centre while most reach the opposing electrode to give rise to a space charge which can affec t following charge injections into the comp onent. The application of an alternating current, which continually reverses the sense of the applied tension, can use these electrons to aga in excite the lumin ous centres in the reverse direction (these electrons accumulate with electrons newly injected throu gh tunnel effec ts from levels localised around the seco nd electrode). The overall brilli ance of these screens remain s relatively low, principally because the source of the elect rons, the semico nductor-insulator interface , has at any single moment a relatively low concentratio n of electro ns and leading to a low availability of electrons for impacts with lumin ous centres. However, the screens are relat ively robust and are widely used as monochrome displays in military applications. In addition, different colours can be prepared. On using manganese ions (Mn2+), introduced by way with zinc sulfide (Mn 2+ : ZnS), a yellow emission at 585 nm can be obtained, a result of the d-d transitions with the breakdown of d-orbitals by crystal potentials. Other colours can be generated from f-f orbital transitions (due to incomplete internal, atomic 4f layer s) in rare earth s. For example, red can be obtained with europium [Eu2+: CaS], green with terb ium [Tb 2+ : ZnS] and blue with thulium [Tm3+, F- ZnSl (see also Chapter VII, Section II for more details).
5 Electroluminescent devices operating under direct current conditions Here, the structures used are either of the metal-in sulator-sem icondu ctor (MIS) or the Schottky barrier type. In both syste ms, the electron source is a metall ic electrode. The structure shown in Figure IX- 18 operates by the passage of electrons throu gh the insulator barrier from the semico nductor valence band (VB)- typically CdStowards a positively polarised metal electrode. The mechanism is equivalent to the
252 Optoelectronics of molecules and polymers
Figure IX-IS. MIS structure with CdS semiconductor.
injection of holes into the semiconductor VB with the following recombination of VB holes with conduction band (CB) electrons. This structure does, however, present two inconveniences: •
•
in the recombination zone, which is placed close to the interface , the interference of defaults, which act as trap levels, results in non-radiative recombinations; and the efficiency of hole injection is very poor due to the competing flow of electrons through tunnel effects from the semiconductor CB to the metal.
In the case of the Schottky junction, an inverted tension is applied (i.e. the metal is negative if the semiconductor transports electrons). Once the tension is strong enough, electrons may be injected through tunnelling effects (barrier triangulation) from the metal to the semiconductor. Thus , a considerable number of electrons can be injected-more than is possible using an alternating tension-and can as carriers collide with luminescent centres such as Mn (transition metal) or rare earths . These devices can function in both continuous and pulse modes, although in the former mode their lifetimes are shortened by a increase in resistivity, a problem which is reduced by using the pulsed mode. (An alternating mode does not give the same problems as it relies upon the structural capacitance). The quantum yields of these devices in the continuous mode is rather poor (n ~ 0.1 %) because of: • • •
the difficulties in obtaining a high enough number of hot carriers to excite the luminous centres; a low, effective sectional area of centres for collisions; and a limited concentration of luminous centres (from 0.1 to 10 %). Above a certain concentration, however, extinction of luminescence occurs due to the crossed relaxation by transfer of energy between luminescent ions (Chapter VII gives further details).
The main advantage of these systems , over those operating under alternating current, is their low consumption of electricity and their relatively easy construction due to their simple structure.
IX Organic structures and materials in optoelectronic emitters
253
VIII Organic (OLED) and polymer (PLED) electroluminescent diodes 1 Brief history and resume The ability of organic materials , both molecular and macromolecular, to be deposited on virtually any substrate, even flexible ones, has solicited the long running and ongoing research into their use as replacements for inorganic semiconductors in a wide range of applications. For a considerable time, the necessary tension required to produce electroluminescence (the required work voltage) of these organic materials was found to be too high for their general use. An example is that of anthracene which required, because of the thickne ss of the crystal s used, an application of around 100 V to operate [pop 82]. However, in the last 10 years, the emergence of new materials based on molecules such as 8-tris-hydroxyquinoline aluminium (Alqj) [tan 87] and on rr-conjugated polymers such as poly(para-phenylene vinylene) (PPV) [bur 90] has got around this problem and has allowed the formation of thin films by evaporation and spin-coating techniques, respectively . More recently, there has been tremendous growth in this technology, stimulated by the economic gains available in the display market. Companies of note are Kodak and Uniax in the States, Cambridge Display Technology (CDT) in Great Britain, Pioneer in Japan, Philips in Holland, Siemens in Germany and Thales and Thom son Multimedia with the CEA and Leti in France.
2 The two main developmental routes There do remain, however, certain problems to overcome before these materials can provide the qualities required for full industrial exploitation. Most important is the fact that, until now, most organic materials have displayed relatively short lifetimes, varying from several hours to several hundred hours , although in some cases several thousand hours . This limitation results just as much from the deterioration of the material s themselves as the degradation in the various interfaces and the electrodes, and depends heavily upon the configuration used in each device [sly 96]. In addition, the material of choice for the emitter has yet to be determined [bar 00], and could be either based on molecules (for example Alq, or more generally speaking q3 type complexes with group lIla metals such as AI, Ga or In) or based on polymers (such as PPV and its derivatives, poly(para-phenylene) (PPP), polythiophene (PTh) or poly(vinyl carbazole), to name but a few). Each material presents both advantages and disadvantages. Oligomers, polymers made up of just a few monome r units, present an interesting advantage in that the maximum emission wavelength can be altered with chain length, given that with changes in their length, their optical band gap also varies [had 00]. Polym ers, meanwhile, generally present a better thermal stability and can be easily processed to give large surface area films, although small molecules can be spread onto large, flexible supports using the 'roll on roll' technique [bur 97]. Materials based on molecules are generally more organised, charge mobilities are higher and function at lower operating tension s. In addition , they are readily purified, resulting in lower numbers of reactions and diffusions at the electrodes.
254
Optoelectronics of moleculesand polymers
For the present moment, both technologies based on molecules or on macromolecules remain important in the fabrication of organic electroluminescent diodes. The terminology used for devices depends on the materials used: the term Organic Light Emitting Diodes (OLEDs) is widely used for devices based on small molecules and Polymer Light Emitting Diodes (PLEDs) is used for those based on macromolecules. For the latter, another term although less used is Light Emitting Polymers (LEPs).
3 How OLEDs function and their interest As detailed above, OLEDs have the advantages of low power consumption (requiring operating voltages of only 2 V) and ease of fabrication (easily formed into thin films or layers). In addition to which, relatively high quantum yield s have already been obtained. Their theoretical maximum yield is 25 %, however, this figure may be eclipsed by recent methodologies which try to circumnavigate selection rules. Given these qualities, it is not surprising that we are now witnessing an exponential growth in the technology and its market [ole 01] . In the following Chapter X, we shall look in more detail at how these organic LEDs actually work, both in terms of theory and practise. At the most fundamental level though, the origin of the optoelectronic properties of these organic solids has been given in Chapters VI and VII. In very general terms, the study of photometric characteristics of OLEDs, in particular their quantum yields but also their lifetimes, are guided by an understanding of the underlining mechanisms of charge behaviours and recombinations (radiative or not) within the organi c material. In classical terms, an OLED can be schematised as shown in Figure IX-19 . The structure used for an organic diode is very different from that used for an inorganic diode. It is not possible to use organic semiconductors in their doped form , which would permit the fabrication of pn junctions similar to inorganic diodes, as doping agents tend to act as extinction centres, 'killing' radiative luminescence [ham 96 and hay 97]. In organic materials, what doe s happen is that the low mobility of the charge carriers is exploited, so that when two charges are injected into the emis sive
Electron injection layer Emission
layer( Iq3. PPV )
Hole injc tum layer ITO (Anode)
/-- - - - --:=::::\-- - - -
Emitted light
Figure IX·19. Typical structureof an electroluminescent organicdiode.
IX Organic structures and materials in optoelectronic emitters
255
layer and come into close proximity, their recombination is inevitable. This is in contrast to inorganic systems in which charge carriers have such a high mobility that recombination centres are required to realise a satisfactory level of recombinations. It is due to the very low mobility of charge carriers in organic materials that there is this gain in a high concentration of optically active recombinations. It is thus useful to study the how organic diodes function in terms offour successive steps : • • • •
injection of electrons and holes at the cathode and the anode , respectively; their transport through one or more organic layers; their association to form a exciton quasi-particle; and the relaxation of the quasi-particle resulting in luminescence.
As detailed in Chapter X, the models so far defined for each of these steps remain controversial. What is probably true is that each type of material , and each type of structure, follows a different system model. For example, current-voltage characteristics are often studied , and explained, in terms of injection either through Schottky effects or through tunnel effects. They can also be interpreted through the so called 'space charge limited' (SCL) current model. In order to reduce the threshold tension for a particular diode, and depending on the dominant process, we should look more to varying the metal of the electrode and the mobility of charge carriers within the organic layers. In Chapter X, we shall concentrate on this physical aspect of the functioning of electroluminescent diodes . The chemical and physico-chemical aspects of these devices have already been covered in depth elsewhere [bar OOa, den 00 and kra 98] so will not be covered in any great depth here. We shall finally concentrate on device applications currently being developed, with special regards to the area of display technology.
x Electroluminescent organic diodes
I Introduction To have an idea of the vast number of articles publish ed regularly on the subject of electroluminescent organic diode s, it is worth looking at the journal ' Synthetic Metals ' , in particular issues devoted to the ' ICSM' conference. While a large number of papers are published in this journal, it shows only a small fraction of all the material available . This Chapter can therefore only limit itself to a very cond ensed view of the subject. Following on from Chapter 9 where the princ iple upon which these device s function was presented, this Chapter : • • •
compares empirically obtained results with those expected from theories detailed in Chapters VI and VII; considers the yields obtained with organic light emitting diodes (OLED) s and the strategies used to improve these yield s; and details the actual and possible future applications of these device s.
This Chapter will not go into discussions on the origins of electroluminescence in organic materials (radiative transition s) as Chapter VII (Section V-4) has already covered an interpretation of the obtained spectra, while Section VI of the same Chapter detailed the nature of excitations (excitons). We have also seen how electron-lattice interactions playa role in these properties, without forgetting the limits of the model, originally proposed for small molecules, when applied to polymer s. For now, we shall ju st give the simple example, as under stood by Burrows et at. [bur 96], that electroluminescence in molecular organic light emitting diodes (OLEDs) is due to the generation and recombination of Frenkel excitons within the Alq3 layer. This was shown by observing lumine scence spectra of Alq3 in solution (in dimethylformamide), which , unchanged from those of solid, vacuum evaporated Alq3, indicated that the recombinations were independent of the molecular environment and originated from excitations localised at individual molecules. These excitons come from both electrons and minority hole s, which control luminescence inten sity, and diffuse through layers which will accept their injection. We shall look at these
258 Optoelectronics of molecules and polymers layers in more detail later on in this Chapter. The electron s are localised at traps, which are themselve s distributed within a gap of average depth E, < ELUMO' These levels come from electron s, which act as polaron s initially placed within the LUMO conduction band (CB) and localised (trapped) at molecule s with relaxation s generating a level with depth Et • Indeed , the shift in the spectrum of electroluminescence with respect to that of absorption can be interpreted as a Franck-Condon displacement, due to the change in the conformation of excited molecule s, while the width of the electroluminescence spectrum can be attributed to strong exciton-phonon coupling.
II Comparing electronic injection and transport models with experimental results 1 General points: properties and methods applied to their study a Properties From the first studies performed on organic solids (using anthracene), it was observed that various regime s of behaviour could exist, especially for example with respect to applied tension. Chapter VI gives further details . However, with OLEDs , clean transition s between different regimes are generally rather rare. Experimentally, we tend more to see only slight variations from the slopes predicted by laws detailed in Chapter VI. Two example s are used in this Section: for the small molecule s, a derivative of Alq3 ; and for the polymers, poly(para-phenylene vinylene) (PPV). The structure in which these materials are presented is simplified to anode/organic solid/cathode, in which either Alq3 or PPV is the organic solid acting as a layer into which both holes and electron s are injected and electroluminescence occurs. There have been published propo sals for distinct mechanisms for each of the material s under study here, respectively, [bur 96] and [par 94], with following and differing proposals, again respectively, [ioa 98] and [blo 97a, blo 97b and blo 98]. More complicated multi-layer structures are discussed in Section V.
b The nature of the electrical measurements and some practical precautions Given that these materials are relatively resistant, it is worth bearing in mind that any measurements must take account of their relatively long relaxation times, of the order of a millisecond to a second, rather than of nanoseconds or less [kar 97]. In practical terms, we can observe in the first characteri stic I(V) curve that there are peaks in the tension which may appear randomly , only to be unobservable on the second trace. These peaks may be due to the filling, during the first trace, of certain deep traps which, statistically, do not empty themselves-and therefore do not need refilling-so that they effectively disappear from the second I(V) trace. It is generally the second curve which is shown.
X Electroluminescent organicdiodes 259 Classically, characterisations are performed by measuring the current flow across a sample to which is applied an increasing tension . The intensity of any electroluminescence is simultaneously recorded (initially with respect to luminance) and the following identification of charge transport mechanisms is made by comparing the empirically obtained I(V) curve against those predicted by theory . The results , interpretations and discussions issuing from this process are presented in the following paragraphs. It is worth noting, however, that there are other important electrical characterisations which may be performed: •
•
•
time of flight measurements which indicate charge carrier mobility (for example, with PPV, at an applied field of 105 V cm- 1, a mobility 11 ~ 10- 5 cm 2 V-I s-I has been observed); measurements of thermally stimulated detrapping, using thermally stimulated currents (TSC) or thermoluminescence (TL), which permit studies of the population of traps and their origin or eventual depth . Using these methods , the depth (U) of traps in Alq3 were determined as U ~ 0.2 eV [for 98] and in PPV as U = 0.35 eV for traps in the volume and U = 0.68 eV and 0.82 eV for the levels of traps at the interface, whose values depended on the polarisation tension [ngu 01]; and dielectric studies which permit measurements of metal-semiconductor barriers for Schottky junctions (using the curve I/C 2 = f'(Vj), or the evolution ofrelaxation phenomena with temperature and frequency to resolve both real (E') and imaginary (E") dielectric permittivities.
Different layers of dielectrics and their interfaces can be represented by equivalent circuits of resistors and capacitors, the values and connections (series or parallel) of which are varied until a near approximation is obtained [jon 83]. For the phenomenon of ideal relaxation, or a Debye dipolar relaxation, for the curve E" = f'(s') we have a semi-circle or flat half-circle (as in the Cole-Cole diagram which corresponds to a distribution of relaxation times), and the presence of a (default) interfacial layer can be characterised by an oblique Cole-Davidson type arc [ngu 01]. While relaxation phenomenon in the volume are dependent on temperature, those due to interfacial layers (next to empty space) exhibit a behaviour practically independent of temperature, as we have already seen in Alq3 . The same material has also exhibited a Debye dipolar absorption with a relaxation energy (U) around 2.3 eV,a value associated with the depth of trap levels in the volume of the material ljeo Olb] . Appendix A-IO gives further details.
2 Smallmolecules (Alq3) a A study of interface barriers in a standard structure oflTO/Alq3/Ca a Principal points The simple lTO /Alq3 /Ca structure simplifies the study of properties of charge injection and transport. The electroluminescent properties, with respect to an electroluminescent diode are, however, relatively limited as although injection, transport and radiative recombinations occur readily in Alq3, the same is not
260
Optoelectronics of molecules and polymers
true for the injection and transport of holes, which control the radiative emissions (thus the necessity of a specific layer added to the anode side in device fabrication) . Thermoelectronic or Schottky [cam 99] or Fowler-Nordheim electrode emissions are generally accepted to be responsible for injection at contacts, when the latter are not ohmic. When the height of the apparent barrier is above 0.6 eV, in general, the current within a structure is thought to be governed and thus limited by these electrodes [she 98]. Once the barrier is lower though, the current is only slightly dependent on the electrode emission (as the contact is on principle ohmic) but is heavily dependent on the volume and follows the laws we established in Chapter VI, where at low tensions the ohmic law reigns and at higher tensions the SCL and TCL laws play their roles. It is interesting to note here how there is a considerable gap between language and reality: an ohmic contact actually results in a non-ohmic conduction law of the type I ex: V'" (with m :::: 2) and is characteristic ofTCL or SCL laws, which reign over virtually all values of tension. The SCL law is exceptional in that between the values of around 0 to I V, typically, the density of injected carriers remains lower than that of thermally generated carriers (which is such that no = N, exp[ -Ec - EF/kT]) . It is only in this minor domain that ohmic characteristics are retained. We shall denote the workfunctions of ITO, calcium and Alq3 as WITO , WCa and WAlq3, respectively, and the electron affinity, the potential ionisation energy and the size of the forbidden band of Alq3 as XAlq3 , IpAlq3 and EGAlq3, respectively. As empirically derived values , we have WlTO = 4.6eV, WCa = 2.geV, XAlq3 = 3.3 eV, EGAlq3 = 2.6eV, and thus IpAlq3 = 5.geV [values for Alq3 obtained from sch 95]. On taking WAlq3 = XAlq3 + (E, - EF), a value calculated from the expression (E, - EF) = kTLn(Nc!no) using Nc = NLUMO = 1019 cm- 3 and no = 1011 cm- 3 (for Alq3 see [bur 96]) , we obtain (E , - EF) = 0.5 eV, that is WAlq3 = 3.8 eV. Figure X-I shows the electron levels prior to the application of a tension . Once contact is made with the electrodes, the positions of bands are adjusted by the alignment of Fermi levels, as shown in Figure X-2 for Vapplied = O. The values of the diffusion potentials at the two interfaces adjust so that Wdiff = WITO - WAlq3 and W~iff = WAlq3 - WCa. In general, we assume that for these organic solids the bands are rigid (oblique, thick grey lines in Figure X-2) and correspond to the metalinsulator-metal (MIM) structure in which there is a constant field across the insulator.
Vacuum reference level
--- --
Wm>=4~
I
-------
---
-- ----
3.3
\ lqJ
r.vc.
W AIqJ = 3.8 I I'AI J= \
E.·
I ITO
r.&:- ~:d.=. 0..5J.f;1 ...... Alq, ~;Alq) =
... _----
.9
=
2.9
E.·
Ca
2.6
Figure X-I. Electron levels prior to application of tension.
X Electroluminescent organicdiodes
Figure X-2. Electron levelsafter contact made (Vapplied
261
= 0).
We should note that a constant potential gradient corresponds to a homogeneous distribution of charges within a volume and that band curvature occurs, typically, in solids in which the concentration of carriers is higher than 10 17 cm- 3 [lei 98, p. 855], and that occurs only for organic solids when they are doped, something not generally applicable to electroluminescent diodes. ~ Electron levels following polarisation On making contact with electrodes and applying a tension of the flat bands, i.e. VBP = (WITO - WCa)/q, we arrive at the situation detailed in Figure X-3 in which the tension VBP = [VITO - VCa] > 0 is applied at ITO and the potential of Ca remains unchanged. Here, the bands are in a rigid conformation and are horizontal after application of the flat band tension VBP (thick, grey lines show the band structure of Alq3 with HOMO and LUMO levels parallel to metal (ITO and Ca) bands and the initial vacuum level) . Once a flat band tension (VBP) and an additional positive tension (Vps) is applied to the anode (ITO), that is Vappl = VBP + Vps, the electron levels take up the configuration described in Figure X-4 in which is represented the resulting band movement.
y Recapitulation of applied schemes (Figure X-5) generally fabricated as detailed in Figure X-5-a .
In practical terms, OLEDs are
Figure X·3. Regimeof flat bands.
262
Optoelectronics of molecules and polymers
Figure X·4. Band schemefollowing polarisation Vappl
= VBP + Vps.
n/V _..VII "\
-"~:-;V~~]-_-.- - -=-:" " - " - 1 =3.3 eV
.z.:fJ ~_ ....
\VITO=
4.6eV
...J '~"" ~
i3 .......
Figure X-5. Practical ITOjAlq3jCa diode: (a) conception; and (b) band scheme.
Given the results shown in Figure X-4, it was possible to prepare the electronic structure shown in Figure X-5-b for the example system. We can see that the drop in tension which appears ofits own accord is in fact what we called VPS (the 'positive supplementary' tension applied to the ITO anode) , and is equal to the total applied tension minus the flat band tension (VFB). The latter is such that VBP = (WITO - WCa)/q. In this example VBP ~ 2 volts, a non-negligible value in contrast to those generally used of the order of 0 to 15 V. Important information can be gained with respect to the interfaces, where the barrier at the anode, seen by holes , is equal to !1A = IpAlq3 - WITO, which in this example is !1A = 1.3 eY. Given the widely accepted value WITO = 4.9 eV, !1Acan be considered to approximate to I eY. Following on from the points noted above at the beginning of this Section, we can imagine that the contact at the anode is not ohmic and risks even being limited by Fowler-Nordheim emissions. We can note though that at the cathode, there is no barrier to the injection of electrons (the drop in potential energy for electrons being !1c = XAlq3 - WCa which
X Electroluminescent organic diodes
263
works out as ~c = O.4eY) . Indeed the contact can be assumed to ohmic as in the region of this electrode the Fermi level penetrates the degenerated Alq3 LUMO .
b Experimental behaviour and first interpretations Studies ofI(Y) characteristics have shown that Schottky emissions can give an ideality factor (n) of the order 20, a very high value indeed, and an unusually high diode series resistance at 50 kQ. However, the emission law for tunnelling effects is not completely verified, even at high tens ions, and contrary to theory it has been experimentally shown to increa se with temperature. In fact, only the TCL law is followed completely within domains which yield electroluminescence (see Figure X-6 for the ITO j Alq3 j Ca structure). The same conclusions as those detail ed just above have been reached, qualita tively, for more complicated system s based on ITO jTPDjAlq3 jMg-Ag by Burrows et al. [bur 96]. TPD is a material used to reinforce hole injection, and Mg-Ag as the cathode has, like calcium, a low workfunction, but exhibit s a slightly lower reactivity [rot 96]. For Burrows et al., interface reactions between the low workfunction electrodes and the electron transport layer (EL) introduce states into the HOMO-LUMO gap and result in ohmic injection at the point of contact. On replacing Mg-Ag with In, which has a higher workfunction, the TCL law is no longer followed and current is not volume limited but controlled by the electrode inject ing electrons. More precisely, the ohmic law is followed at low tension s (due to thermally generated carriers of density no) in thick films, while the SCL law is followed in the same regime for thin films (current varies as y 2 j d3, so when d is large, the current is dominated by the simple ohmic law) . As the tension increases, the Fermi pseudo -level rises and traps start to fill up. This decrease in the number of empty traps, which now receive few electrons, induces a rapid increase in mobilities and the overall current, resulting in the TCL law being observed (I ex ym+ I j d 2m+ I) . At a sufficiently high value of V, all traps are filled and we should once again find the classic SCL law, although this type of value of V is rare ly obtained without destroying the films.
(a) (b )
.018 .014
~
80
...c
60
.~ III
.01
-
...
E
'Q
oS
~
... '"c .s'" c 3
40 20 .002
o
o
5
10
15
20
0
0
V o ltuge ( V)
5
10
15
20
Figure X·6. (a) leV) characteristics of the ITO/Alq3 /Ca structure; (b) Luminescence curve with tension for the ITO/ALq3/Ca structure.
264
Optoelectronics of molecule s and polymers
There have been numerous arguments developed as to why the TCL law is observed [bur 94] and [bur 96]: • • •
•
when m is sufficiently high , I <X V Id 2 , so that when I is a con stant , V = f(d 2 ) is a straight line as indicated in Figure X-7-a; as T, = Et /k = mT ,mmustincreaseasTdecreases,again showninFigureX-7-b; additionally, m = Tt(l/T) , and plotting m = f(l/T ) gives T, = 1780K and Et = 0.15 eV which is a value in agreement with that given by quantum calculations (0.21 eV and detailed in Chapter IV, Section III-3 (see also Figure X-7-c)); taking the law I <X Vm + 1Id 2m+ l , it is possible to determine N, = 3 x 1018 cm- 3 and N, = 1019 cm- 3 (also using the formula for Jexp given in Chapter VI, Section IV-6-b). In addition, from the volume mass, the density of molecular sites can be evaluated to the order of 2 x 1021 cm- 3. We can conclude that electrons injected into LUMO levels are subsequently strongly localised and with a high proportion of which being held in trap levels, from which they can recombine (radiatively) with holes; nevertheless, their low concentration with respect to the overall number of molecular sites can explain their low quantum yield in Alq3 (around I %). Figure X-7-d gives a general view of the mechanism of electroluminescence.
(b) I (A)
10.3 (a) ~
10"
iZO
05
10
c
10-6
~c 15
07
10
~
10-1 09 10
010
m
=
10
10011
( d) ~ - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - i
: I
• Franck • Condon
...In
,I, L...:....:..:= Il ol, InJm lon
(e) m
15
10
and dlfTlLu on :
t..- 40OI.,.
..:<;..""T'!'-#"""'-"---"'''"'----....:j /
E•.e'
..-.-
..
10
Electro n injection and TeL current Op tical ga p: 2.7eV
: I
:
: : I
a
Recofhblnatlon zone ~ - - - -------- - - - - - - - - - -- -- - - -- - - - --- ----- - ---
Figure X-7. (a) Line V = f (d2 ) in which d
== film thickne ss. (b) I(V) curves with varying T. (c) Line m = f(l /T) in which the slope gives T" that is Et = kT t . (d) Electroluminescence mechanisms in Alq3.
X Electroluminescent organic diodes 265 An 'academic' hypothesis ofthe TCL model operating with the trapping time being longer than the average transit time (for a hop between two molecules in the LUMO) was proposed to answer criticisms concerning electronic transport in the model, which envisages a band structure arising from the solid (see discussion in Chapter VI, Section IV-2-a). The mechanism of transport limited by traps (TCL) simply demands a sufficient delocalisation of charges to establish a thermal equilibrium between free and trapped charges [bur 96]. As we have seen, N, ~ Ne , indicating that each electron introduced into the LUMO band will subsequently and automatically trapped on an Alq3 molecule . A relaxation would follow yielding a polaronic state which would then result in conduction occurring through hopping mechanisms appropri ate to these quasi-particles (with reduced mobility, as experimentally confirmed with Itn ~ 5 x 10-5 cm 2 V- 1 s"),
c Controversial points and proposed improvements [ioa 98] a Controversial points [ioa 98] under discussion: • •
There are essentially two details which remain
that concerning the actual existence of the band scheme for small molecules , although this argument is not discussed here; and that which relates to the hypothesis of invariance of mobility with respect to an electric field, which is used in establishing the SCI and TCL laws. There are the following considerations which can be brought to mind: - up until now, because of the low mobilities and short mean free pathways (mfp) observed in organic solids, it was thought that between any 2 collisions the carriers could not gain much energy from an applied field, and that mobilities and transport were governed by temperature (T) through thermal vibrations overcoming barriers and were essentially independent of the applied field (in contrast to inorganics) . - However, in disordered systems, the general expression for It is empirically obtained and has only been verified through Monte Carlo simulations in terms of position and energy for individual jumps between disordered sites [bas 93]: It
= Ito exp (~2~~) exp ( C {[k;
r-}:2} E~/2)
in which Ito is the mobility in a zero field, a and}: are parameters which characterise, respectively , the energetic (diagonal disorder) and positional (non-diagonal disorder) degrees of disorder [cam 98b] and [shi 98], while a represents the width of the Gaussian distribution of transport states and t}. = 2a/3 . Alternatively, Gill's empirical law for charge transfer, established using amorphous complexes is also used [gil 72]: It(T, Ea ) = Itoexp
A),
(-~) exp (G kT kT eff
eff
where
T eff
.!.T -To
266
Optoelectronics of molecules and polymers
in which ~o is the activation energy at zero field, To is the temperature at which straight lines J.1 = f (I IT ) with respect to the applied electric field gives an intersection (experimentally, these lines converge at l iTo) . Generally for small molecules, the derived mobility of carriers increases with the applied field. In the presence of energetic disorder, the electric field aids electrons overcome potential barriers due to energy differences between sites, which affect mobilities [ioa 98]. The mobility follows a Poole-Frenkel like law (which works over concentration-see Chapter YI, Section YI) of the form:
from which vananons with temperature can be obtained by placing 1: = 1:oexp(-~ /kT) into J.1 = qt / m. However, in certain materials such as polymers doped with molecules to the order of 5 to 25% by mass, mobilities do decrease above a certain value of the applied field Ea. As shown in Figure X-8, in qualitative terms, we can suppose that this effect is due to 'diagonal disorder ' associated with the variable distances between molecules [gre 95]. Under a weak field, there are many available and facile pathways (short distance hops in different directions with respect to the field) which are, nevertheless, removed once a strong field is applied . ~ Possible models The presence of trapping levels has been shown not to be necessary by Conwell's group, by modelling the characteristics of organic materials [ioa 98]. The group has even supposed that such levels do not exist, because in examples where only electrons have been injected (using the same LiF/AI contacts on either side, which are supposedly ohmic), the I(Y) curves are identical whether or not the tension is interrupted during the measurements, indicating negligible electron trapping. We should consider, however, the kinetics of such an experiment-see the preceding Section II-I-b. Experimental characteristics may be verified simply by using Ohm's law, into which can be included the appropriate law for variations in mobility: J.1 = J.1o exp(aE~ /2) where J.1o is the mobility under a weak field and a a parameter increasing with disorder. This has been found to be true when using 1= ne ~Lo[exp(aE~/2)]Ea, with a = 1.3 x 10- 2 cmo.s y- o.s and J.1o = 6.5 x 1O- lOcm 2 y - 1 s-l).
Electron trajectory under weak field: collisions are
disorientated and electron folio"... energetically favourable path, Transport ilio not dependent on pecitional disorder,
Under a strong field, collision: arcorientated andelectronh3..~ enforced trajectory . On meeting a barrier. electron passage is arrested nd mohilit',' decreases when r~ is verv hi2h.
E : siro n!: field
'IJf\
~
E
A
weak field
+
Figure X-S. Qualitative description of charge transport in strong and weak fields.
X Electroluminescent organic diodes
267
Its important to state though that the presence oftrapping levels has been confirmed using a variety of techn iques: •
•
Thermo-Stimul ated Luminescence (TSL ) [for 98] in which the principal peak was modelled using a distribution of traps with energies between 0.25 eY and 0.15 eY. Two supplementary peak s were obse rved toward s lower energ ies (around 0.07 eY); and Photodipolar absorption [jeo 0 Ib1 which results from a thermo -photo -die lectric effect due to: - a photonic, preliminary luminescence exci tation with elec tron ' pumping' onto trap levels (typica lly with a Wood lap emitti ng light at ). = 365 nm); - a thermal effect with an initial cooling then heating of the sample; and - a dielectric effect by reorientation of dipoles associated with trapped charges using a radio frequency field.
Thi s technique has given rise to traps with depth s of approx imate ly Et = 0.2 eY, and has shown that trap s can persist, following excitation with daylight , for around 1 hour. It seems reaso nable eno ugh to assume that effec ts due to space charges and mobil ity dependencies on the applied electric field should affect J(Y) charac teristics [she 98]. However, if we look close ly at these charac teristics with respec t to TCL representations (which is the most wide ly respec ted law), then we can see that they do not follow perfectl y straight lines. There is very possi bly an improve ment which can be made to the TCL law by taking into accou nt mobil ity dependence on other parameters such as tempera ture and the electric field. If we look again at the general expre ssion for current density, ignoring the diffusion term, we have J = pv = qnu.E , that is, J = qn~ Y/ d. In general, as above disc ussed , the concentratio n n of current limited by space charge are in the form n ex V'" . Once only free (untrapped) charges contribute to the space charge, then m = 1 (giving the saturation current J, in Mort-Gurney' s law). If charge space is dominated, however, by trapped charges (as can be supposed given the above detai led results) within traps of expo nential energy distribution, we now have m = Tci T where E, = kT c . As detailed above, we now have J ex y rn + 1, and in addition, if we suppose that mobility (u) is not actually a constant, the J(Y) law will depend on variatio ns in I-l and will no longer follow a law based on y rn + 1, if ~ varies with the electric field, that is with Y/ d (where there is a break with the TCL law). The esse ntial problem is to reso lve the dom inant effec t (space charge or mobil ity) in any specific tension domain . If we can suppose that mobi lity varies negligibly with respect to E a , so that Laplace's equation may be integrated, we can direc tly introduce the appropriate mobil ity law I-l (Ea , T) into TCL type equations.
3 Polymers a Initial models [Par 94] Emissions through tunnelling effec ts (Fowler-Nordheim) In the ca se of poly (2methoxy,5-(2' -ethylhexoxy )-para-phenylene vinylene), commonly called MEH-PPY,
Ct
268
Optoelectronics of molecules and polymers
Parker showed by experiment that carrier injection is controlled by the height of the electrode-polymer barrier. For the demonstration, diodes which gave preferential injection of one charge carrier type over the other (see Figure X-9) were used. This effect is classically obtained by varying differences between the workfunction of the cathode metal and the electron affinity of the polymer on the one hand, and the workfunction of the anode metal and the ionisation energy of the polymer on the other. In so doing, at the metal-polymer interfaces, one can favour the passage of holes and destroy that of the electrons, as shown in Figure X-9-a, or indeed favour the passage of holes and destroy that of the holes , as in Figure X-9-b. With MEH-PPV, the best results have been obtained using a calcium cathode and an indium tin oxide (ITO) anode. Experimental curves have shown that the I = f(V) curves: • •
uniquely depend upon the value of the electric field (and not the tensions, as is found for Schottky inorganic structures); and are virtually independent of temperature.
This behaviour can be seen as characteristic of tunnelling effect, following the FowlerNordheim equation, over a triangular barrier. Log(I/E;) = f(I/E a ) is a straight line, and permits a deduction of the barrier heights at the interface between the injecting electrode and the polymer (for ITO see Figure X-9-a, and for Ca see Figure X-9-b). This conforms with the scheme for rigid bands as the bands curves can only be at a minimum given the low carrier density within the polymer, estimated to be of the order of 10 14 cm- 3 from C(V) measurements. ~ Functioning voltage and yield Generally speaking, I-V characteristics are essentially determined by the majority carrier, which are in turn determined, be they holes or electrons, by the lowest electrode-polymer barrier, respectively, situated between the anode and the polymer or between the cathode and the polymer. However, the yield of a diode is determined by the minority carriers injected at the highest level of the barrier, a parameter which we will look at in more detail below. Indeed, the
Vacuum level 2.8eV
Ca
1-::=== f-
4.geV
Anode (+)
Organic film (a)
In Al
f----C
A
Cathode (-)
Anode (+) Organic film Cathode (-) (b)
Figure X·9. PLED structure favouring: (a) hole; and (b) electron injection.
X Electroluminescent organic diodes
269
yield can be varied by changing the barrier observed by minority carriers, and this can be done without modifying the function voltage (the barrier observed by majority carriers). The inverse is also possible. On going from ITO to Ag and then to Ca, as shown in Figure x-tO-a, the anode tension must be increased so that hole injection can be maintained (respectively, 10, 15 and 25 V). The slopes of the bands ensure that tunnelling effects are as large as the workfunction of the metals are low. There is an optimised yield when the barrier observed by minority carriers is zero , as in Figure X-tO-b, i.e. the barrier at the cathode is as low as possible. However, the lowest functioning voltage is obtained when a zero (minimum) barrier is observed by the majority carriers (at the anode) . Diode optimisation is generally accepted when the chosen electrodes are such that the workfunction of the anode is equal to the ionisation potential of the polymer, and that the workfunction of the cathode is equal to the electron affinity of the polymer. For the system here, using MEH-PPV, the best pair of electrodes are thus ITO for the anode and calcium for the cathode (See Annex A-II, Section II-I for the description ofMEH-PPV). The yield is around I% for a field of approximately 3 x t0 7 Vm - 1• We can remark that the barrier observed by holes is around 0.2 eV, and for electrons is near 0.1 eV, and that the role s of majority and minority carriers has been reversed. It has been shown the yield can be improved when using Ag as an anode, and at the cathode, with Sm (2.7 eV) or Yb (2.6 eV), the operational voltage does not decrease and chemical reactions between the low workfunction metals and the polymer may occur-risking the formation of interfacial barriers. y Starting andfunction tensions The starting voltage depends only on the band gap of the polymer, and would be equal to this gap if it were not for non-zero barriers at the interfaces (see Figure X-II-b). The tension does not depend on the thickness of the polymer film-as verified by the characteristics shown in Figure X-II-d. The minimum voltage required for the diode to function-that is to produce tunnel effects and emit a visible light-as shown in Figures X-II-c and d, does however depend on film thickness, as the tunnel effect is a current fixed by the field, which has a value
Figure X-IO.(a) Effectson tunnellingat the barrierdue to workfunctions; and (b) an optimised component.
270
Optoelectronics of molecules and polymer s
PP V
Ca
PI' /
" 2..J' cV ITO /
eVappl
ITO ------~~ . _ - - - - - -
(a ) Zero bias (V,\ l' = 0); no tu nneling,
(h) Flat hand condition: lInsl'l mltllgl' for tunneling to uccur; eVrll=\Vn o • \" eo = 1.11 -v ( = El:l'r, ' if harrier at electrodes is zero ),
------
(cjf'or ward bias: Tunnelling injection uf both carrier types,
IlIgl~47S ,
, ,,
00 , 1200 (1I)
Ohmi c zo ne
L:!::::========~_L8JiL..-_-.llIg V Figure X-ll. Band structures ofITO / PPV / Casystem: (a) zero bias; (b) at flat band condition; (c) forward bias; and (d) corresponding log I = f(logV) characteristics.
dependent on film thickness. The minimum functional voltage is sensitive to barriers at the electrodes, in contrast to the starting voltage which would vary directly by ,OJ eV for a barrier of 0.1 eV, as detailed in Figure X-II-b.
b The roles of current limited by space charges (SCL), traps (TCL) and double injection (VCC) Bradley and his team have shown that for PPV used in the simple set-up ITO IPPV I Al [Cam 97], the Fowler-Nordheim law did not correctly account for experimentally obtained results with respect to temperature, film thickness and the amplitude of I(V) characteristics. At high tensions, the law observed was of the TCL type , with an exponential distribution of traps of average depth of 0.15 eV. At lower tensions, the law followed was space charge limited (SCL) , exhibiting a mobility which varied with temperature and field in accordance with the Arrhenius law. The transport through the volume can be seen as a hopping mechanism between states distributed following a Gaussian curve , with deep sites playing the role of traps. Another study, run simultaneously to that detailed above and following the same idea as that detailed previously [par 94], was carried out in the Philip s laboratories [Blo 97a , Blo 97b and Blo 98]. The Fowler-Nordheim law gave rise to currents considerably higher (by several orders) than those found experimentally. Two mechanisms were studied, those of hole and electron transport. Here we will describe each individually.
X Electroluminescent organicdiodes
271
a Hole transport Using the ITO/PPY/AI structure, which favours hole injection only, it was shown that current followed the SCL law, as shown in Figure X-12-a. We have Is = (9/8)£l-lp y 2 /d 3 , showing that current is volume and not electrode limited. With s = 3, hole mobility could be estimated as I-lp = 5 10- 11m 2y- 1s-l . It should be noted thatat high fields, a deviation from the SCL law occurred (experimentally, the current was higher than that given by Js, as shown in Figure X-12-b). As detailed above, because of 'non-diagonal' disorder associated with variable distances between molecules, under low fields facile transport pathways are available (short hops in directions at variance with the applied field) which become inaccessible at higher fields. As the field strength increases, the mobility follow s a Poole-Frenkel type law (assuming that traps are not responsible for disorder, as there is a quadratic SCL regime without traps unlike the TCL system). With I-lo the mobility under zero field and /::". the energy of activation, I-l = I-lo exp( -/::". /kTo) exp(aE 1j 2) . This gives /::". = 0.48 eY and I-lo = 3.5 x \0-3 m 2 y-I s-I. The factor a has been empirically defined with respect to temperature as a = G
(k~
- k+0)' The insertion of I-l into Js has been used to obtain
an excellent agreement with experimentally obtained l(Y) curves . Here, G = 2.7 X \0-5 eYYo,s m-o,s and To = 600 K, values similartothose obtained forpoly(N-vinyl carbazole) (PYK). We should note again , however, that to obtain Js from the SCL law, we have to suppose that I-l is a constant with respect to x, but E = E(x), so we have to state that the variation is sufficiently small so as to be able to perform the integration!
B Electron transport The example used here is that of Ca/PPY / Ca which favours electron transport and is shown in Figure X-13 . The current due only to electrons is less than that due only to holes, up to 3 orders at low tensions , Limited by traps, electron current is strongly field dependent, and follows a TCL law, that is J ex: yl+ l / d 21+ 1, in which traps are exponentially distributed, The slope of log J = f (log Y) gives m and T, = 1500 K and N, = 10 18 cm - 3 . y Recombinations On the basis of bimolecular recombinations, mechanisms involved in recombinations have also been studied [Blo 97a] . The I(Y) characteristics
r'
E
P'
s..,
E
..,s
0.1
10 V (V)
0.1
10 V ( )
Figure X-12. (a) SCL I(V) curves at Tambient ; and (b) deviation from the SCL law at low temperature and under a high field,
272
Optoelectronics of molecules and polymers
~::c/~/ /4m 221m
10'"
10
100 V (V )
Figure X-l3. I(V ) characteristics for electron transport. give rise to only a slight difference bet ween single hole and double injections. Double injections are hole dominated while electrons are highl y trapped. The recombination con stant has been estimated to show that only around 5 % are actually radiative, the greater part in PLEDs occurring non-radiatively.
III Strategies for improving organic LEDs and yields 1 Scheme of above detailed proces ses Figure X- 14 detail s the vario us stages towards electroluminescenc e [Bra 96]. To give a summary of the different stages, covered above: •
A in which currents {I} (elec trons) and {2}(holes) are injected, respectively, giving rise to leak currents {I' } and {2 ' }. Figure X- 14 shows curre nt densities and carrier speeds;
[Cd Materiulair interface [U)
Figure X-14. Basic mechanisms in electroluminescence.
X Electroluminescent organic diodes 273 • •
•
B in which electron-hole recombinations occur, resulting in the initial formation of excitons in singlet {3) and triplet {4) states ; C in which excitons are dissipated either through the radiative {6) (singlet ~ singlet) or non-radiative (7) (singlet ~ extinction centre) and {8} (triplet ~ singlet) pathways; and D in which there is refraction of the light beam on going from the material to air interface.
2 Different types of yields As detailed in Chapter VIII, in general terms, different types of yields may be defined as:
a The external quantum yield This yield, the external quantum yield, is defined by: Il ext
=
number of photons emitted outside the structure . . = T]EL· number of Injected charges
The external quantum yield can also be thought of as the product of two other yields: T]ext = T]opt T]<jlint. where T]<jlint is the internal quantum yield and Ilopt the coefficient given in Chapter VIII to account for refractions at the diode-air interface (step D in Figure X-14) . With an organic material with an indice n greater than that of air, only internal emissions incident to the interface at an angle below the limiting angle 8\ can escape towards the exterior. The result is a non-negligible loss, as the factor T]opt ~ 1/2n 2 (calculated in Chapter VIII, Section 1II-2, using Lambert emissions) is of the order of 0.2 when n = 1.6. External yields are therefore only around 20 % of internal yields . Efforts required to improve this figure are detailed later on.
b The internal quantum yield The internal quantum yield can be thought of as the product of three different factors . Each one is with respect to the steps A, Band C, detailed in Figure X-14, and can be singled out in the defining equation for this yield, T]<jlint = YT]r
•
Y is the level of recombination of injected carriers i.e. Y = Jrlh. In Step A, with JT = Jh + J~ = I, + J~ (total current density) and Jr = Jh - J~ = Jc - J~ (recombination current density) then Y = ) if there arc no leak currents a~ = J~ = 0) and there is an exact equilibrium between the two types of current, i.e. Je = Jh. However, for example, if all holes are used up in recombinations, J~ = 0, then some electrons will traverse the whole structure without recombining giving J~ =1= 0, and Y < I; T]r is the generated fraction of radiative singlet excitons, as denoted in Step B, due to the probabilities of the spins required to yield electroluminescence from
274
•
Optoelectronics of molecules and polymers singlet states (S = 0, Ms = 0) and triplets (S = 0, Ms = -1 , 0, 1). 11r can be directly estimated from 11r = us /[Us + vrl = 0.25 = 25 %; and <1>[ is the fluorescence quantum yield (see Step C) and while always below I, it can reach up to 0.7, the loss being due to inevitable, non-radiative recombinations {7}. The latter are due to singlet excitons recombining, in general, close to the interfaces, or because of the presence of extinction centres such as impurities and non-radiative traps . In addition, bimolecular recombinations do not operate at 100%, even with the low mobility of carriers in organic media.
c The quantum energy yield The quantum energy yield is expressed in W W- 1 and represents the ratio Emitted luminous energy
hv = 11EL- Supplied electrical energy - nchargeseV eV
11 -
-
nphotonshv
From the above equation it is evident that for a given emitted wavelength (given hv), the lower the operational voltage, the higher the energetic yield. This explains the interest in trying to reduce the operating voltage . Typically, organic materials exhibit values of hv/ev of around 0.3.
d The luminous yield The luminous yield takes into account the photo-optical respon se of the human eye, which is defined by the relationship 11L = 11 . K(A.) in which K(A.) is constant relating observed and actual scales of energy.At A. = 555 nm, K(A.) = 683lm W- I . This yield is thus expressed in lumen watt" I .
3 Various possible strategies to improve organic LED performances Luminance, which depends on the intensity of emitted light , is determined principally by the current density of minority charge carriers and then by the number of these carriers which undergo radiat ive recombinations with the majority carriers. The quantum yield , which can be written as the product of the four terms detailed just above 11EL = 11 opt 11<1> int = 11 opt Y11 r
the highest number of minority carriers undergoing radiative recombinations. This in turn necessitates the use of efficient electrodes and injection layers for these carriers (with a high injection current or ohmic contact). Given that interfaces tend to favour the presence of defaults, which act as extinction centres of luminance, it is judicious to try and displace the recombination zone for the minority carriers towards the bulk of the material. This necessitates the use of a minority carrier transport layer, as the injection layer may not necessarily be good for minority charge transport ;
X Electroluminescent organic diodes
•
•
•
•
275
an improved method for allowing otherwise trapped emitted light to exit the device . Microcavities, structures which diffu se light , can help direct the emi ssions and impro ve the otherwise highly detrimental value of lIopt; as high a possible level of injected carrier recombination . y = Jr/Jr will increase if: - Jr is large and , as previously noted , there is as great a current of minority carriers as possible, which in turn demands as Iow a leak current as possible. The use of layers confining the hole s and electrons can respond to this demand; - Jr is small and therefore the majority current is not too great with respect to the minority current. The injection of majorit y charges which do not go on to recombine with minority charges adds nothing beneficial to the optical behaviour of the device, uselessl y consume s current and results in a harmful heatin g effect which reduces its lifetime [tes 98]; the highest possible level of radiative exciton production possible (i .e. a high value of lIr). This in turn means recovering the highest possible percentage of triplet excitons which result in electron injection. The use of phosphorescent materials and mechanisms which can transfer triplet to singlet states can be envisaged; and the fluorescence quantum yield (f) should be as high as possible. Generally, in the solvated state , this factor can be very high , even near to I (for example, laser dyes). However, in the solid state, this value is generally much lower, typically of the order of 0.1 to 0.5. Thi s is due to forbidd en dipolar transition s between the fundamental and lowest excited states which appe ar, either localised on a dimer or as a band in the solid state, following the breakdown of degenerate levels present in the solvated state [sch 00] . Thu s well organised and crys talline states should be avoided, as we have already see n in Chapter VII, Section VI-6. There is nevertheless a condition that can be imposed upon the latter remark, and that is that any disorder impo sed should not be so great as to limit any gains in transport (injection and that of minority charge carriers) which can arise from the organi sation of a system (where charge mobility can be high) and would otherwise impro ve the fluorescenc e yield . Thi s is a characteristic of certain types of material s, for example those based on discotic molecule s [seg 01]. In addition, as previously mentioned, non-radiative centr es should be excluded, by the use of layers free of structural faults or other imperfe ction s.
Another, delicate problem is that of ageing, which results from external effects or from the electrodes. The former may be resolved using encapsulation, while the latter is slightly more difficult but can be resolved using barrier layers, an example of which is PPX deposited via VDP (see Chapter VII, Section 1-3). There is no way we could even pretend to detail all the possible strategies that have been devised to answer the above criteria. Instead , we shall limit this Chapter to only the most currently used solutions, especially when we look at actual appl ications of these devices. Nevertheless, we shall briefly detail why some organi c solids are p-type (polymers such as PPV or poly(pa ra-phenylene) (PPP» and why others are n-type (small molecules such as chelates), at least when protected from oxyg en.
276
Optoelectronics of molecules and polymers
IV Adjusting electronic properties of organic solids for electroluminescent applications 1 A brief justification of n- and p-type organic conductivity a Small molecules The best known example is Alq3, in which the chelation, or complexation, of the AI3+ ion with 3 ligands leaves the aluminium reduced in electron density to become effectively an electron acceptor. When assembled with other Alq3s, this character results in a facile transport of electrons, and thus Alq3 is considered an n-type material. Another example is that of layers of the complex rare earth complex of diphtalocyanine PC2M, where Pc is [C32HI6NS]2- and M is the rare earth ion. These materials are intrinsically n-type (under vacuum) . Scandium diphtalocyanine is paramagnetic, as its outer orbital is but half-filled and has unpaired electrons delocalised over the phtalocyanine macrocycles. The n-type conductivity, under vacuum, can be due to intermolecular transfer of these single electrons. On contact though with oxygen, the gas is cherni-absorbed and forms oxygen- PC2M bonds . The oxygen cannot be removed by the simple application of a vacuum, due to the formation of a charge transfer complex in which the PC2SC is lacking in electrons and the oxygen gains a negative charge . The positive state of the PC2SC moves as a hole through diphtalocyanine molecules which surround the negatively ionised oxygen molecule. In effect, these materials change to being p-type once exposed to air, as do many polymers which are subject to a similar mechanism.
b Polymers In general, polymers tend to behave as p-type semiconductors. The origin of this can again be contributed to the presence of oxygen [gre 94, p 58] . We can also add that in the case of PPV, obtained like many other polymers from the thermal conversion of a precursor, that the process used for its preparation can give rise to many pendent bonds. A possible result is therefore the transfer of electrons through the corresponding levels, also possibly generated by thermally diffused oxygen, from levels at the highest point of the polymer valence band . The latter thus generates holes. The generation of this p-type character of polymers can also be evidenced on doping using ion implantation [mol 96].
c Adjusting the type of conduction The type of conduction of a material can be changed by altering the 'backbone' of the organic material, simply by adding on electron donating or accepting groups (see also Chapter XII, Section 11-3). For example, PPV can be modified to facilitate : •
the injection of electrons by increasing the electron affinity (X) of the polymer on adding electron attracting groups, such as cyano (CN), onto its backbone.
X Electroluminescent organic diodes
277
Figure X-IS. Structure of cyanated poly(para-phenylene vinylene) (eN-PPV).
•
Figure X-IS shows the example of eN-PPY [bra 96]. Even aluminium can be used to replace calcium as the cathode with this material, without altering the yield; the injection of holes by stabilising their presence on the polymer by modifying it with electron donors such as alkoxy (-OR) or amine (-NH2) groups.
2 The problem of equilibrating electron and hole injection currents As detailed above, the equilibration of electron and hole injection currents is essential in order to generate excitons. If this cannot be done then: •
•
a large current of electrons or holes can pass through the device without generating excitons, an obligatory step in the process of light emission, thus reducing the yield; and there is an initial formation of excitons only to be reduced in the neighbourhood of one or the other of the electrodes (the cathode or the anode if, respectively the majority current is holes or electrons) in a process tied to the presence of default extinction sites of the organic-inorganic interface. There are two methods by which an equilibrium can be reached (Figure X-16) :
•
•
adjust the workfunctions of the metallic electrodes so that the barriers at both organic-inorganic interfaces are close, in a method only valid if the current is determined by injection and not by the bulk. However, this can mean the use of reactive electrodes, which suffer from problems which will be detailed in Section 3 below ; and modify the organic solid to the workfunction of the metallic electrodes so as to reduce the size of the barriers at the two interfaces. Electron affinity and ionisation potentials are parameters used to choose appropriate materials, although the choice is also governed by the type of transport.
3 Choosing materials for electrodes and problems encountered with interfaces A very simple and conventional structure is illustrated in Figure X-16, into which PPY or Alq3 can be placed .
278 Optoelectronics of molecules and polymers ......................... _.-
.......»:
--_._.._._..._. ·.. .t
....
Ca
IT
Figure X-16.Modification of electrode and bulk materials in a simple system.
a At the cathode Briefly : •
•
Metal from the cathode can diffuse into the polymer, which becomes doped. The injection barrier is therefore moved to between the doped and undoped parts of the polymer. Covalent polymer-metal (aluminium) bond s can develop with the generation of a barrie r toward s charge injection at this level; Different alkaline-earth metals have been used with Alq3 . With Ca, it is apparent that the presence of residual oxygen (10- 6 mbar durin g deposition ) forms a passivation layer which arrests interactions (Ca with N then a of Alq3 if Ca is deposited on Alq3), or degradations of Alq3 (if Alq3 is deposited on Ca). With Mg as the cathode, oxygen needs to be completely removed. However, the injection barrier at the interface of Al and Alq3 is actuall y reduced if a thin layer (0.5 nm) of LiF (or CsF) is introduced between Al and Alq3 . The introducti on of a thin layer ( I nm) of MgF 2 between Alq3 and an alloy of Mg:Ag ( 10: I) increa ses both the quantum yield and lifetime.
b At the anode The most typically used substance for the anode is mixed indium and tin oxide (ITO). It has a square resistance between 4 and 80Q /D. An inconvenience which does arise with this material is its ability to generate oxygen, which can diffuse toward s the organic solid and result in a degradation due to photo-oxidation. The p-type character of conjug ated polymer s makes them good candid ates as material s for anodes, favourin g the injection of holes. They can also play a role in protecting against oxygen . Interesting effect s were observed with doped polyaniline, which being opticall y transparent was used to replace, or used on, ITO. As we shall see, in multi-la yer structures, polyethylenedioxythiophene (PEDOT) can also play the role of barrier against diffusing oxygen and hole injection if (J > 2 Q-I ern" I , as can copper dipht alocyanine .
X Electroluminescent organic diodes
279
•
v + eII.nod< /......... /
////
Confinement zone (exciton
formatlon )
O --f=-~
Exnmple
ITO
PPV
C -PP
Ca
Figure X-I7. Confinement zone formation.
4 Confinement layers and their interest It was very quickly realised that confinement layers were necessary to improve the probabilities of carrier recombinations [fri 92], even though organic materials provide high probabilities due to the relatively low carrier mobilities . The use of this layer though also allowed greater separation of the recombination zone from the electrode interfaces. As shown in Figure X-17, the confinement zone is obtained by choosing materials which at their interfaces form barriers against holes coming from the anode and against electrons coming from the cathode.
V Examples of organic multi-layer structures: improvements in optoelectronic properties 1 Mono-layer structures and the origin of their poor performance As an example of a mono-layer structure we will detail ITO/Alq3 /Ca. Figure X-5 shows that while electrons may be easily injected at the cathode towards the emitting layer, as there is no potential barrier, a similar remark cannot be made for holes . The high potential barrier, around I eV, which holes observe at the interface between anode and Alq3, reduces any charge injection. This can only be overcome by the application of a high potential, which results in charge transfer, notably, by tunnelling effects . As previously discussed, luminance and electroluminescent yields are strongly dependent on the minority current. With the Alq3 molecule being n-type, the difficulty found in injecting holes explain s to a greater degree the poor luminances obtained with mono-layer structures. To reduce these problem s, different types of layers can be used and there are examples of di-Iayer, tri-Iayer, and even multi-layer structures.
280
Optoelectronics of molecules and polymers
2 The nature of supplementary layers Independent of the nature of the emitting organic layer (the organic material used original in a mono-layer device) , various other layers can be introduced. Generally speaking, these layers can be termed: • • • •
Hole Injection Layer (HIL); Hole Transport Layer (HTL); Electron Injection Layer (ElL) ; and Electron Transport Layer (ETL).
The following paragraphs detail the way in which these layer s function and will exclude descriptions of the operation of chemical groups from which they come, a subject covered elsewhere [bar OOb]. Appendix A-I 0 does however give the chemical formulae for molecules and polymers from which the layers are formed . HIL and HTL layers are particularly necessary when the emitting layer is made of a small molecule such as Alq3 which favours electron transport. When the emitting layer favours hole transport, for example with polymers and notably PPV, it seems reasonable that to aid minority carriers, electrons injected at the cathode, ElL and ETL layers should be used. Here , we will study only examples relating to small molecules. It is worth adding that, as we have seen in Chapter VIII, there are effects associated with different physical treatments of the emitting layer, which can be similar to those obtained using various chemical layers . We shall see in Section 4 that the densification by ion beam assisted deposition of the emitting zone in contact with the anode can augment up to 10 times optoelectronic performances of OLEDs.
3 Classic examples of the effects of specific organic layers [tro 01] a HIL layer effect The HIL layer is in contact with the anode . One of its many roles is to perfect the planeness of the interface, reducing effects caused by points which otherwise locally rupture the dielectric field. Another of its roles is to act as a barrier against impurities, notably oxygen, which diffuse from the ITO anode towards the organic emitter. If allowed through , oxygen gives rise to premature ageing of the organic layer and non-radiative centres may be formed . The most widely known material, which fulfils this role, is poly(3,4ethylenedioxythiophene) doped with poly(styrene sulfonate) (PEDOT-PSS) and it can be prepared as a film using spin coating. Alternatives, although less efficient, are available in the form of copper phtalocyanines. In order to study the benefits of using an HIL layer, optimised structures of ITO /AIQ3 /Ca/AI and ITO/PEDOT-PSS /AIQ3 /Ca/Al have been compared. It was found that the monolayer structure had a performance which was considerably improved upon by the bilayer structure. As shown in Figure X-18, the luminance for the former was 49 cd m- 2 (at 18.0 V) while the latter displayed greater than 5000 cd m- 2 (ate .a. 9.2 V). The threshold voltage, in the same order, dropped from 8.0to4.1 V,
X Electroluminescent organic diodes 10000 Luminance (cd rn-
281
z)
1000
~
50 nm PEDOT+ 60 nrn Alq3
-SOnrnAlq3 100
10
Tension (V) 1 +------h------f.~...------.-----___.
o
5
10
20
15
Figure X-IS. L = f(V) characteristics for ITOjAlq3 jCajAI and ITOjPEDOT-PSS jAIQ3 j Caj Al structures.
Eo No electron confinemen t
--- ---------
) •I 3.1 eV
Ia
~ z.s ev
I I I I
4.7eV
I Hole confinement
I 5.2 eV
---------- --------
ITO
I
t
/
~/~ ~
5.66 eV
Ca PEDOT Alq3 (HTL I - - - -- ''I'lIl, ...
2
n
- - PEDOT-PSS
Figure X-19. Band scheme of the ITO/PEDOT-PSS/ AIQ3/Ca structure.
while the quantum yield improved from 0.02 to 0.72 % (luminance yield increased from 0.02 to 0.991m W- 1) . In Figure X-19 it is evident that the band schem e of the bilayer ITO/PEDOT-PSS /Alq3 /Ca/Al structure has the PEDOT-PSS HOMO level lying in between that of Alq3 and the workfunction of the anode AlQ3 ' permitting hole injection into the structure. There is also a confinement of holes at the PEDOT-PSS /AIQ3 interface.
282 Optoelectronics of molecules and polymers
b HTL layer effect This layer is generally deposited in between the HIL and emitting layers. The materials used for this layer are either sublimed small molecules such as N,N' -diphenyl-N,N'-(3-methylphenyl)-I, I' -biphenyl-4,4'-diarnine (TPD) or polymers such as PVK, which may be deposited using spin coating. These materials display relatively high hole mobilities (J.Lp ~ 10- 3 cm 2 V-I s-I) and have a HOMO band quite close to the Fermi level of ITO. In the bilayer structure of ITOjTPDjAlq3jCa, as detailed in Figure X-20, we can see that on the one hand, the intermediary level of the TPD HOMO level aids hole injection into Alq3, while on the other, the LUMO level appears as a sizeable potential barrier at the TPD j Alq3 interface . The latter stops electrons from going from Alq3 to TPD and confining carriers. Thus at the same time the TPD layer generates more holes and more electrons in the Alq3 layer, increasing the number of radiative recombinations and improving the luminance from 49 to 9600 cd m- 2 , as shown in Figure X-21.
c Trilayer structures Individual studies of the effects of HIL and HTL layers on diodes have demonstrated that: • •
the HIL layer allows lower working voltages; and the HTL layer permits confinement of electrons and holes at the HTL/Alq3 interface.
2.2geV
4.7 eV
t ITO
5.37 eV
.. f'.
!e2.g ev
I 3.1 eV I I I I I I
:x f 5.66 eV L~
TPD
Alq3
Ca
Figure X-20.Band scheme for the ITOITPDI Alq3 lea structure.
X Electro luminescent organic diodes
10000
283
Luminance (cd m" )
--tr-
1000
40 nm TPD + 60 nm Alq3
-e- 20 nm PVK + 60 nm Alq3
-
80 nm Alq3
100
10
Tension (V)
1+-----r-----+.......--I---~----"""'T"----
o
10
5
15
20
= f(V) characteristics for ITO/ Alq3/ Ca/ A1, ITO/ TPD/ AlQ3/ Ca/ AI and ITO/PVK/ AlQ3 /Ca/ Al structures.
Figure X-21. L
Figure X-22 -a shows how a structure ca n be made to combine the effec ts of both of these layers. Th e resu lts, shown in Figure X-22-b show that this optimisation can give rise to a luminance of arou nd 22500 cd m- 2 (at 12 V). Th e worki ng voltage actually used can be optimi sed by varying the thickness of the various layers [tro 0 1].
(a)
2.29 eV
Co nfinem nt
~
2.9 eV
TPD
Ca
4.7 eV 5.2 eV
ITO PEDOT
Figure X-22. (a) Band scheme of the ITO/PEDOT-PSS /TPD/ AIQ3/Ca / AI (2) structure, (b) L
= f'(V) characteristics of bi- and tri-Iayer structures.
284
Optoelectronics of molecules and polymers Luminance(cd m-2)
(b) 20000
-e- 40 TPD + 60 Alq3 -e- 50 PEDOT
15000
-
+ 60 Alq3
40 PEDOT + 20 TPD + 60 Alq3
10000
5000
O. . .- -....... ~~iIEii&iiiiiiiiiiiiiiiiiiiiiiilfOl~~::.,.--..:=~
o
5
15
10
20
25
Figure X-22. (Continued)
4 Treatment of the emitting zone in contact with the anode While physico-chemical treatment of the anode (ITO ) using oxygen plasma can lead to an improvement in organic LED performances, we have seen that treatment of the actu al emitting zone can also improve the injection and tran sport of minority carriers lead ing to an increase, by an order of size, of the luminance and yield of a LED . The effect of this treatment is detailed in Chapter VIII , and here it suffices to present a 1.2
ITO/Alq y'Ca --ITOIP30T /Alq y'Ca ITO/Alq ) assisledlAlq)/Ca
~...
.~ 0.8
f. 'I. /
v"".
..
.....
0.6
~
= ':r
]
.. ·V-
I
......
v
.
E
§
---,
----
-
0.4
~I .I /
\
-,
•
]
..
0.2
I
,i
~
o .......-..-- ................ J....-r-::;'--.A 0
10
15
20
25
30
35
Vo lt age ( V)
Figure X-23. Quantum yields for mono-layer, chemical bilayer and physical bilayer structures, in order of increasing yield. .
X Electroluminescent organic diodes
285
comparison of the yields obtained by three different structure s in Figure X-23 . These three structures are: • • •
a single layer ITO/Alq3/Ca structure; a non-optimised 'c hemical bilayer' of ITO/ P30 T/ Alq3/Ca, in which P30T plays the role of the HTL layer, preferentially transportin g holes; and a 'physical bilayer' of ITO/ 25 nm Alq3 depo sited using ion assistance /50 nm Alq3/Ca, where the assisting beam was of helium ions with energy 100 eV and current density j = 50 nA cm- 2 and the period of assisted deposition was optimised at ~t = 100 s.
The advantage of the physical bilayer is that it require s only one single chemical product to be evaporated, however, the technique does necessitate an ion source and cannot be applied to OLED s prepared using vacuum sublimation.
VI Modification of optical properties of organic solids for applications in electroluminescence 1 Adjusting the emitted wavelength There are several ways in which the wavelength of the emitted light can be varied: •
The size of the forbidden band varies with the conjugation length n of a polymer (or oligomer). When n is increased, for example in going from an oligomer to a polymer, there is a global evolution in the number of interacting states and thus a decrease in the size of the forb idden band. The result is a shift in emissions to the red. Inversely, the use of oligomers shifts emissions towards the blue. In the case of PPP, an empirical law has been given detailing the absorpt ion peak (Eo) [lei 98]: 3.16] Eo = [ 3.36 + ~ eV ,
•
•
which explicitly shows how, for example, when n decreases, on using oligophenylenes, Eo increa ses; when monomer units within a polymer gives rise to weak Jt interactions (overlaps), for example between phenyl rings, the resulting gap is large. For example, PPP is a good candidate for blue emissions as its gap (emission peak at 465 nm) is greater than that of PPV (peak at 565 nm). The introducti on of non-conjugated sequences, which dimini sh the degree of conj ugation, has been used with PPVs to induce a blue shift in the emission. MEH-PPV, PPY modified with alkoxy group s (used by CDT, Cambridge) emits at 605 nm (in the orange-yellow); on turnin g to small molecules, we can see that the most widel y used are organometallic comp lexes, for example based on a central metal ion such as beryllium, magnesium, zinc or gallium and an outer set of ligands which act as
286 Optoelectronics of molecules and polymers
R = H: 8-hydroxyquinoline (q) R = CH 3 : 2-me thyl-8-hydroxyquinoline (mq)
Bebq-
lO-hydroxybenzo[h]qu inoline (bq)
Figure X-24. Representations of Alq3 and Bebqj along with the ligands q, mq and b.
•
emitters (as we have seen in the case of Alq3) . The emission wavele ngth for these spec ies is generally towards the green, but can also be modified slightly by using a different metal cation, thus altering bond lengths with the ligan ds. For example, we have }. = 530 nm for Alq3 and}, = 517 urn for Bebqj , as show n in Figure X-24. Blue gree n and even blue colo urs can be reached by displacing the em itting zone towards TPD, for exa mple. The central ion can also be a rare eart h, giving rise to a change in the emitted wavelength. This is discussed further in Section 4. Another strategy consists of grafting small electrolumi nescent molecules onto polymers [gau 96]. Various possi bilities have been explored, using varying concentrations of dye, such as coumari n. Alone, these dyes have a tendency to crystallise , thus loosi ng efficiency. The problem remains though that such structures requ ire high starting tensions and do not appear to be particularly stable.
2 Excitation energy transfer mechanisms in films doped with fluorescent or phosphorescent dyes Studies of host-guest systems, Alq3 (host) - DCM2 (2% guest fluorescent dye) and Alq, (host - PtOEP (8% guest fluorescent dye), have shown in both cases that exci tations are formed directly on the host Alq3 syste m [bal 99] . However, the emissions of the guest syste ms are very strong, and in the forme r syste m less than 1% of emissio ns come from Alq3. This indicates a high level of excitation transfer from the host towards the guest.
X Electroluminescent organic diodes
287
(a)
(b)
---+-== - - ----.~-
~---~ Fig ure X-2S. Transfer of excitation energy from a host molecule (D: Alq3) to a fluorescent dye guest molecule (A: DCM2). (a) Single host ~ singlet dye fluorescent transfer; 10* + 1A ~ 10 + 1A * Both Forster and Dexter transfer possible, but former is more important (b) Triplet host ~ triplet dye fluorescent transfer; 30* + 1A ~ 10 + 3A * Only Dexter transfer possible here; with fluorescent dye, phosphorescence is only slightly possible.
Gi ven the re sults detailed in Chapter VII , Section VI -7 co ncern ing mechanisms of excitation transfer, we can sum marise the po ssible energy transfer proce sse s from the ho st (D for donor) to the guest (A for acceptor) for a fluorescent dye (Figure X-25 ) and for a phosphorescent dye (Fig ure X-26). If the two mechani sm s, Forste r and Dexter
,
(a)
i) lot
'At~
...
lot~
,i 'A*
-ll.. Internal Iconversion I
'ot~
3
t A*t
~
(b)
_jt_ '0
Figure X-26. Transfer of excitation energy from the a host molecule (D: Alq3) to a phosphorescing dye guest molecule (A: PtOEP). (a) Singlet host ~ singlet phosphorescent dye ~ triplet phosphorescent dye transfer; I D* + I A ~ 10 + I A*. Forster and Dexter transfer are both possible, but the former is more probable. The following internal conversion, I A * ~ 3A *, relaxes radiatively as A phosphoresces. (b) Triplet host ~ triplet phosphorescent dye transfer ; 30* + 1A ~ 101 3A *. Only the Dexter transfer is possible between D and the phosphorescent doping agent A, which radiates.
288
Optoelectronics of molecules and polymers
transfers, are allowed in a given system, then the Forster transfer normall y dominates, due to its ability to act over long distances.
3 Circumnavigating selection rules: recuperation of non-radiative triplet excitons a The problem As detailed in Chapter VII (Section V-3-a), following an injection of electron s, three triplets states appear for each singlet state. In fluorescent material s, only emissions from the latter state occur radiatively, and more or less instantan eou sly, in a relaxation to the fundamental state, which is generally also a singlet state. Three quarters of excitons occur in the triplet state, which principally undergo non-radi ative relaxations, and therefore it is evident that for electroluminescent applications these excitons should be recovered so that they can relax radiatively. Phosphore scent materials can be used to do this. On modify ing the (spin) symmetry of a system, the triplet state s disappear slowly through radiative recombinations. It is this slow decrease in luminescence which corre spond to phosphorescence. While admittedly this method is not highl y efficient , the phosphor escence can be improved by the presence of heavy atom s favourin g spin-orbit coupling, mixing triplet and singlet states. However, there are almost no useful phosphorescent organic material s, which have, however, given rise to a vast choice in fluorescent material s.
b Initial, poorly efficient solution s: a phosphorescent layer and Dexter transfers An initial solution to recovering energy associated in electroluminesce nce with triplet excitons is the introduction, in an organic LED, of a supplementary layer containing phosphorescent material [bal 00 and sam 00] . However, as we have mentioned, there are very few organ ic materials which can generate from their triplet exci ted state a significant pho sphor escence. In additi on, the slow declin e of triplet states in the phosphorescent layer leaves open the possibility of a transfer of these triplet states to triplet states in the fluorescent layer (Alq3), which are non-radiative. In practise, in a donor-acceptor system, where the fluorescent acceptor directly dope s the phosphorescent donor materi al, only transfers over short distances can occur. Forster type transfer s are unlikel y; Dexter transfer s occur more readily due to the proximit y of acceptor and donor molecules, and exciton s hop from one molecule to the closest neighb our simply by overlapping molecular orbitals. The transfer of energy from triplet s states (phosphorescent molecule ) to singlet states (fluorescent molecule ) is highly unlikel y, as the mechanism of hoppin g over short distance s conserves symmetry over the donor-acceptor pair, and only transfer from the donor triplet state to the same triplet state on the acceptor can result. Once excitons reach the acce ptor triplet state, in terms of radiation efficien cy, they are lost as the fluorescent dye can only yield a negligible phosphorescence.
X Electroluminescent organic diodes
289
A change in spin orientation, thus assuring a transfer from triplet to singlet states, is only possible if the donor exciton relaxes before reforming at the acceptor, following a random exchange of electrons. This mechanism though remains improbable as the required disassociation of the donor exciton requires a high amount of energy-of the order of I eV in molecular systems.
c Multi-layer systems and Forster transfers As we have already seen, there remains an alternative transfer mechanism. The Forster transfer is associated with long distances, around 5 nm, and does not require contact between molecules, and permits changes in spin of transferring excitons [bal 00]. Chapter VII, Section VI-7-b gives further detail s. In addition, in order to transfer excitons from a host material to an excited singlet state on a fluorescent dye, a phosphorescent and organometallic intermediate is required. Thus, both singlet and triplet states from the host material are transferred to the phosphorescent intermediate, which in turn allows transfers to the singlet states of a fluorescent emitter, which in turn works radiatively in an efficient manner. So that these transfers are possible, the exciton observes a reduction in its energy at each step, much like a ball descending a stairway and as schematised in Figure X-27. The phosphorescent dye, in this configuration, stimulates the transfer of energy from the host material , which acts as donor, to the fluorescent dye acceptor. The transfer is in effect step-wise. However, the concomitant non-radiative Dexter transfer (illustrated by crossed out arrows in Figure X-20), which permits the passage from the triplet state of the phosphorescent intermediate to the triplet state of the fluorescent emitter, should be limited if not completely suppressed. A near total suppression can be accomplished by using an emitting layer itself consisting of alternate layers of phosphorescent intermediate and fluorescent emitter both diluted within a host which ensures the sought Forster energy transfer. Once any
... X- - - - -
-~
'X, ... Triplet :
Sing let
hv
Non 1'Idi. live
Funda menta l
level
.-----..., ,...------, hosphorescent intermediate
Figure X-27. Schematisation of Forster transfer mechanism (full line), where the phosphorescent intermediate stimulates energy transfer from the donor host material to the acceptor fluorescent dye. The internal conversion is detailed as a dotted line, while Dexter type transfers are shown as dashed lines. Dexter transfers-to elimitate-are schematised as dashed lines crossed out. After [bal 00].
290 Optoelectronics of molecules and polymers fluorescing dye singlet is formed, its radiative fall is immediate. This helps to reduce the total number of excitons in the system at anyone moment and, by consequence, the risk that they would transfer towards a triplet state and extinction . A widely used material for the host electron donor layer is a dicarbazolebiphenyl called CBP. Typically, the phosphorescent intermediate is iridium tris(2phenylpyridine) otherwise denoted Ir(ppy)3, and the fluorescent dye is often DCM2, a red dye. Complete chemical formulae can be found elsewhere [bal 00]. With an optimised structure, which contains a considerable number of transport layers of both holes and electrons, external quantum yields greater than 3% have been found, a multiplication by four of that obtained from the fluorescent dye alone. Another advantage of this configuration is that it does not rely upon phosphorescent emissions, which permits the application of molecules which are not necessarily phosphorescent as the phosphorescent intermediate [sam 00]. We can also note that the increase in radiative yield decreases the number of phonon descent processes, which in tum diminishes losses due to heating and, accordingly, increases LED lifetimes. There is however a cost, and that is that as the energy transfer descends towards lower and lower levels, and the resulting emissions are mostly in the red, sometimes in the green and with extreme difficulty in the blue. This tends to limit the number of available applications for these systems . In the fabrication of electrically pumped lasers we can see that this technique can be used to limit losses due to reabsorption of light emitted by triplet excitons . In addition, this by-passing of selection rules can be useful not only to optimise the number of singlet excitons produced but also in order to prepare organic lasing diodes.
4 Energy transfer with rare earths and infrared LEDs a Ligand-rare earth transfers at the heart of chelates The name chelate encompasses a group of compounds consisting of multi-dentate ligands attached to a central cation . Co-ordination bonds between the ligands and the cation are formed by the ligands donating electron pairs. As already detailed for the chelate Alq3, the standard chelate for electroluminescence, the emission colour is determined by the ligands with a peak at 525 nm. Doping with dyes can induce blue or red emissions. On inserting a hole transport layer at the anode side, luminances as high as 10000 cd m- 2 have been reached with yields of 1.5 lm W- 1 . Photoluminescence or electroluminescence can be obtained from chelated rare earths, attached to ligands by single or double bonds . Gadolinium yields UV light, while cerium gives rise to the colour blue. Terbium gives green, europium shows red, dysprosium displays yellow and erbium emits in the infrared . Figure X-28 schematises the basic mechanism. Either by photoluminescence or electroluminescence, respectively from incident photons or electron injection, ligand electrons are excited from a fundamental singlet to an excited singlet state from which relaxation results in fluorescence. Triplet states are also occupied due to excitation by electroluminescence . The excited states, whether they be singlet or triplet can go on to transfer energy to energy levels associated with the rare earth 4f orbitals, as long as Crosby's
X Electroluminescent organic diodes 291 L1GA, ... D
sing
nonra d ali ve
Figure X-28. Rare earth ion excitation by organic solids.
rule is respected [Cro 61]. This states that the lowest energy level of a ligand triplet state in the complex should be close to equal or just above the resonance energy level of the rare earth ion. A difference of 0.05 eV is sufficient to ensure a 95% photoluminescence yield . On emitting light or through non-radiative processes, the rare earth ion can then relax to its fundamental state . It is interesting to remember that when a ligand is excited from its fundamental state, 25% of the resulting states are singlets and 75% are triplets . All this energy can be transferred to the rare earth ion, which means that there is a potential internal quantum yield of 100% [Bel 99]. In these chelate systems, it is the rare earth which is responsible for their lifetimes and the wavelength of the emitted light. The ligand though is responsible for the absorption, the power of the emission and , in practical terms , the ease of handling. ELAM, a company in London, indicates that yields obtained with these systems can be up to 60 to 70lm W- I , which can be compared against that of fluorescent tubes at 100 1m W- I . OPSY, a company in Oxford, UK, has announced luminances of 200 cd m- 2 in the red and green, with photoluminescent yields of 80%.
b Infrared organic LEDs [Gil 99] Following purification, sublimation of a methanol solution of erbium chloride and 8-hydroxyquinoline can give films of erbium tris(8 -hydroxyquinoline) (Erq-), Er3+ exhibits a strong luminescence centred at 1.54 urn due to a transition from the first excited 4113/2 state to the fundamental 4115/2 level. Light at this frequency is within the window of transparency of silicon based optical fibres, used in communications. Using the OLED structure glass /ITO/TPD(50 nm) /Erq3(60 nm)/AI, photoluminescence around 1525 nm and electroluminescence around 1533 nm was obtained. Secondary emissions were also found and attributed to isomers of Erq3' There are certainly difficulties with respect to yields, and only qualitative results have been published (i .e. graphs with arbitrary scales) . The size of the difference in
292 Optoelectronics of molecules and polymers energy between radiative recombinations at the ligand s, which persist in Erq, and the 4113/2 ---+ 4115/ 2 line may explain these results.
5 Microcavities A typical structure is made using a Bragg mirror inserted between a glass substrate and a layer of ITO (98 nm and with n = 1.8), onto which a layer of PPY is deposited (160 nm). Aluminium or silver electrodes function as a semi-transparent mirror, as shown in Figure X-29-a. The photoluminescence spectra, like the electroluminescence spectra exhibit considerable narrowing of the spectral curve (having a width of only around 5 nm half way up) with respect to that of PPY obtained in free space [Tes 96]. The intensity of emissions permitted by the cavity are also increased greatly, and even more so when using silver as the mirror as it allows less losses than aluminium (Figure X-29-b) .
6 Electron pumping and the laser effect For the OLEO s so far detailed, the current densities are of the order of I to 10 rnA cm- 2 for luminances of around 100 cd m- 2 . For lasers, higher densities are required , but they are a priori limited by low carrier mobilitie s so that at high injection levels absorption increa ses. The use of tetracene (4 join ed phenyl rings) has allowed relatively high mobilities-at least for an organic solid!-at around 2 cm 2 y - 1 s- 1 to be attained. Amplified spontaneous emission by optical pumpin g was observed in the middle of the 70s [Pop 82] in anthracene and doped tetracene. More recently, a lasing effect by injection has been reported [Scho 00]. For the latter, tetracene was used in a perfect crystalline form in order to banish defaults and impurities otherwise insupport able in optoelectronics. Vapour phase deposition was used to give crystals of around I to 10 urn thickness and I mrrr' surface area. Two field effects at the electrodes were used to ensure an equilibrated injection of holes and
ITO DUR
(a)
Glass subs trate
Figure X·29. (a) Microcavity structure; and (b) general shape of photoluminescence curves.
X Electroluminescentorganic diodes
293
. :3
- VI Grid 1
1
<8> Figure X-30. (a) Cross sectional view of structure; and (b) schematisation of grid-source tensions applied to give field effect injections.
electron s (see also this point developed in Section l-b in this Chapter). Figure X-30 schematises the fabricated structure for this device and shows the two field effect electrodes used to inject charges. To describe the device we will refer to this Figure . Around the crystal there were deposited a source, a drain, a dielectric grid and a grid, with the former two for hole injections made from gold, while aluminium was used to inject electron s. Holes were injected by the application of a negative sourcegrid at the upside and electron s were injected at the lower side by the application of a positive tension between the source and grid deposited on the lower side. The field effect acts much like a variable doping at the contact s with the crystal, and the concentration of carriers can be varied by adjusting the grid tension. Between drain I and source 2, and source I and drain 2, a tension was applied (around 5 V) to a slice of the crystal allowing electrons and holes to traverse the device, respectively, upward s and downwards. Electroluminescence and amplified stimulated emissions are detected laterally. In addition, the organic crystal can play the role of waveguide, but the grid dielectric here is too thin at 150 nm to act as a coating . In fact it is air which plays this role, allowing only a multi-mod al guide. Cleavage of the crystal faces, which have a reflectivity of 8% can induce a Fabry-Perot type resonance. At a value Vg = 50V, carrier densities of 1013 cm- 3 were estimated using measurement s of capacity and variations in tensions and thus conductivities. A potential drop of 5 V held between the high and low points of the structure assure current flow. As a consequence of injection, excitons are formed and light emissions are observed. At a temperature of 5 K, three peaks were observed for a very low pulsed current « 1A cm - 2 ) . The peaks were characterised as being due to radiative transitions between first excited and fundamental states and included vibronic levels (0- 1, 0-2 .. . transitions). They were separated by 170 eV, a value corresponding to intramol ecular vibrations. As shown in Figure X-31, an increa se in current density, by increa sing the grid-source tension, gave rise to a dominant 0-1 band with a mid-height width reduced to lOmeV at a density of 30 A cm- 2 . At j > 500 A cm- 2 , a vertical line appeared, of width less than I meV. This abrupt narrowing of the spectral line at a threshold current of 30 A cm- 2 is typical of a spontaneously amplified emission with the contributed guidance gain. The second drop at j > 500 A cm- 2 corresponds to the start of the lasing effect.
294 Optoelectronics of molecules and polymers J~ Wid!h_o!~IU.i~ion
_100 (meV)
"
band at mid-height \
\ \
-10
-1 I
1
\
<,
-I
--,
\
\
\ \ \
\ 1'-
10 100 1000 current density (A em")
Figure X·31. Emission line width at mid-height and at 5 K with respect to the function of pulsedcurrentdensity (l0 I1S, 100Hz).
VII Applications in the field of displays: flexible screens 1 The advantages One of the potentially most interesting developments, in industrial terms, is the fabrication of flexible displays and screens . It was realised , right from the start of the development of screens with pixels made from OLEDs and PLEDs, that they had numerous advantages . (Recalling the term, pixel comes from the contraction of 'picture-element' , while interestingly in French the word 'eldim' would be used, a similar contraction of the words 'element d'image' .) When compared to liquid crystal displays (LCDs), they have the advantages of giving a wider angle of view (Lambert 's emission) , a higher luminance (several 100,000 cd m- 2 have been attained) , an extremely high commutation speed, a low minimum working voltage around 5 V, low levels of energy consumption and no need for back-lighting. There have been plans to use OLEDs as back-lights and white diodes have been prepared for the lighting market. We will first say a few words on white diodes , before looking more in depth at the realisation of screens.
2 The problem of ageing Ageing determines the lifetimes of LEDs [Ngu 98 and Miy 97]. The definition used to qualify the lifetime of a device is the time it takes for the luminance to descend to one half of its original value [Si 97]. The measurement can be made using either of two methods . In one the applied tension is kept constant, and in the other the current which traverses the device is retained constant. Figure X-32 shows the results obtained using the latter method . The original luminance is fixed at around 100 cd m- 2 . The tension and the luminance are measured every 30 seconds so that the curves L = f(t)
X Electroluminescent organic diodes Luminance (cd m-
z)
30 nm CUPC + 60 nm Alq3
I
295
Voltage (V)
14
120
12
100
-Luminance -Voltage
80
10 8
60 6
40
4
20
2 Time(h)
0
0 0
Figure X-32. L
3
= f(t)
6
and V
9
12
15
18
= f(t) characteristics of the ITO/CuPc/ Alq3/Ca/ Al structure.
and V = f(t) can be traced . The example structure shown, ITO/30nm CuPc /60nm Alq3/Ca, has a half-life thus estimated as 12 hours . Outside of problems due to breakdown, which can result from an inhomogeneous film, migrations from the electrodes towards the layers can occur, stimulated by field effects. As examples we can cite metallic indium which comes from ITO, as does oxygen which can go on to modify chemical groups , most notably those which fluoresce. At the cathode we can blame oxygen and water vapour for the appearance of black points localised about defaults which were there to start with and just go on growing . Another participating fault is no doubt that of crystallisation of active layers due to heating . This is the reason why there have been numerous works published concerning the treatment and improvement of electrodes and interfaces, most notably those of ITO. An example of one treatment is that of subjecting an ITO surface to oxygen plasma for 10 minutes which results in an improvement in its workfunction and this an improvement in hole injection. The roughness and the resistance of the ITO surface are also improved using this method and the overall yields are improved [Kim 99]: Finally it is worth mentioning the unavoidably necessary process of encapsulation of organic LEOs. Different approaches have been used: that of sealing between two glass plates and a ribbon of glue; and encapsulating within a polymer barrier layer such as PPX or one of its chlorinated derivatives deposited using VDP (see Chapter VIII for further details) . In common with all electrical components, organic diodes need to be fabricated a priori in a dust free ' white room ' so that the lifetime required for industrial applications is attained, which at present is of the order of 10,000 hours . Indeed, on an industrial scale, the fabrication of specific layered devices requires the connection of individual chambers each operating specifically to a certain layer. At the present moment, each company will have without doubt its own proper techniques.
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Optoelectronics of molecules and polymers
3 The specific case of white diodes Uniax, within the EEC, has fabricated PLEDs for lighting purposes which have photon to electron yields between 2 and 3% operating at 3 to 4lm W- I at a low applied voltage . The luminance is better than that obtained from incandescent or fluorescent lamps . As ever though, the problem remains lifetimes, mostly due to heat. In a pulsed mode, luminances close to 100,000 cd m- z have been reached. If initial yields of25% can be attained, not an entirely unrealistic value, then this area awaits considerable development. Figure X-33 schematises the 'intelligent' layering of emissive layers with each emitting in the visible region . The ordering of the layers is made with respect to the type of injected carriers and the direction of emission, towards the emission window, so that successive absorptions do not occur. In effect, the layer nearest to the window should have the largest band gap [101 97 and Miy 97].
4 The structure of organic screens One of the advantages of organic LEDs is their very short communication time . Inversely, that also means that their remanence is very short lived. So, in the case of multiplexing, where sweeping of each line of pixels is required (as in passive matrices) and so the screen gives an acceptable average luminance (from around 100 to 200 cd m- z for a television), the luminance at anyone moment needs to be very high (n times the number of lines swept, for a screen with n lines) . The lifetimes of LEDs functioning under such conditions is therefore well reduced. The use of active matrices therefore becomes inevitable. They also offer a gain in resolution. This change in direction is also justified by the fact that OLEDs are particularly well suited to individual addressing, which can be performed via a polycrystalline silicon FET, although organic semiconductors can claim also to be perfect candidates as materials for the commanding transistors [bur 91 and hor 00]. In Figures X-34-a and -b, respectively, are shown a schematisation of a MIS field effect transistor (MISFET), which has a semiconducting channel made from PPY implanted with iodine ions (E = 30 keV, D = 4 x 10 10 ions cm- z) and its characteristics. This transistor operates in the accumulation phase, with the gate voltage being negative with respect to the p-type semiconductor finally obtained [Pic 95] .
~
Cathode Al
.... ... ~
,r
Blue
(yrcc1
Red
Glass
.
Multi-laver Iq3 (40 nun ) Alq3: i1eRed 1% mor 1(5 om) Alq3 (5 om ) TAZ (3 om ) TPD (40 om ) TO
Figure X-33. Schematisation of a white LED with the required order of layers.
X Electrolum inescent organic diodes
PPV
297
(a)
gam
16 g t: <3 c
4
1---------.__
~ 2
~
~
0 ..............·-
-8
-
_
.·
-6 -4 ·2 SourcclDrain Volt age (V)
cathode
Alq TPD
ITO
Figure X-34. (a) Configuration used in a polymer based MISFET transistor (after [pic 95]); (b) Ids = f(V ds) characteristics following Vgs for a MISFET with an iodine implanted PPV semiconductor channel; and (c) schematisation of a completely organic pixel.
Figure X-34-c shows the general constitution of a completely organic pixel from a monolithic integrated polymer FET and an organic LED [Bao 99]. The ITO, placed against the substrate, makes the LED anode while a photographically imposed layer of gold defines the gate electrode of the FET. The insulator for the gate is a layer of Si3N4 which is about 180 nm thick . The semiconductor, poly(3-hex ylthiophene) (P3HT) is a regio-regular polymer helping give it a high charge mobility at around 0.002 cm 2 V -I s -I. Above this is the drain and the source and the channel is about
298
Optoelectronics of molecules and polymers
5 urn long and 1 mm wide . The drain is joined to the anode of the LED, which is of a classical bilayer structure and has en external yield of about 0.4%. The maximum current through the LED is 50 itA cm- 2 (equivalent to a current density of 72 rnA cm- 2 ) . The luminance of such a pixel has been estimated at 2300 cd m- 2 , a value well above the 100 cd m- 2 necessary for display applications. An all polymer pixel has also been described, in which PPV replaces Alq3 and polyimide replaces SbN4 as the dielectric grid. As for the deposition techniques used, we can say that small molecules are deposited using evaporation under vacuum and polymers are spread using spincoating. The technique of ink-jet deposition which has appeared is particularly adapted to polymers, while there are also techniques based on 'roll-on-roll' for small molecules [Bur 97]. It is interesting to consider that while colour screens require the three colours red, green and blue (RGB), the necessary materials have been identified (although need some improvement [den 00)), and that all is required is juxtaposition of the three types of pixels using techniques particular to organic solids, which are not that removed from those currently used in microelectronics [Bar OOa and Bar OOb].
5 A description of the fabrication processes used for organic RGB pixels Research into improving OLEDs lifetimes to greater than 10,000 hours with initial luminances of more than 300 cd m- 2 also stimulated a development in the technology surrounding their use, specifically, in flat screens . To fabricate the RGB pixels, various technologies were tested, particularly to try and avoid etching based techniques: • • •
development of white diodes which emitted through RGB filters; use of blue diodes (i.e. at the highest energy required) which excited phosphors emitting in the green and red; and adjustments, using micro-cavities, of emissions from a wide band organic emitter.
However, for the above systems, the power emitted was limited, and the use of three individual layers for each colour was found to be indispensable. This required the fabrication of sub-pixels using etching techniques: • •
' wet' technology using solvents, either acids or water, which nevertheless generate problems associated with the induced degradation of the active organic materials; 'dry 'technology in which pixels are obtained using plasma etching, which a priori, presents no specific problems due to degradation.
In order to obtain high resolution screens, anodes and cathodes necessarily should be made to a precise geometric form, and this in accordance with the structure of the pixels on the screen which are either deposited in a matrix of points or as segments . The ITO anode is the most facile to prepare, using either 'dry' or 'wet' etching techniques being done before any organic layer is deposited. For the cathodes though, which demand an extremely high degree of geometric precision, their fabrication requires extreme care . In reality, the materials used for the cathodes (AI-Li or Mg-Ag
X Electroluminescent organic diodes
299
for examples), can be deposited directly onto an organic layer using 'wet' etching, however, when the organic layer is one which is fragile and sensitive to thermal or solvent induced effects , then particular steps must be taken. The literature proposes various routes, depending on whether small molecules or polymer s are involved, and below we shall look at some of the possible methods .
a For layers from sublimed molecular materials: use of aT-form cathode separator [Nag 97] The technology should allow for the fabrication of OLED devices which have dimensions around I urn . The technique involving T-form cathode separators was used by Pioneer to realise their first commercially available screens . The separator between pixels, sized around 30 urn , was prepared prior to depositing the organic layers and the metallic cathode. Practically speaking , the cathode is fabricated around the T-form separators in three steps, as shown in Figure X-35. The cathode separator is shaped in conical form and has a retracted base-as shown in Figure X-35-a . It can be obtained using a negative working photo-polymer-the irradiated part of which resists etching development-by relying on the cumulated exposure with depth . The photo-polymer, deposited by spin-coating, exhibits properties similar to those of a photo-resin
substrate (a)
substrate (b)
(c)
Figure X-35. The three stages in diode fabrication via a T-form cathode separator: (a) elaboration of the cathode separator; (b) evaporation of organic materials at an oblique angle with respect to substrate ; and (c) evaporation of the metal cathode at a angle perpendicular to the surface.
300
Optoelectronics of molecules and polymers
Photo- oolvrner
...,..... 1'h00o·oolvmer
Substrate (a)
Substrate (b)
Slow development 4 "" Fnsl development
Figure X-36.Realisation of the phasegivenin FigureX-35a: (a) spreading thephoto-polymer; (b) selective exposure throughmark; and (c) development.
with additional properties in development speeds and exposure time. As shown in Figure X-36, a longer exposure time can result in a more noticeable removal of material. The T-form of the separator can also be obtained using a double polyimide/Siolayer deposited on the anode (polyimide on the anode then SiOz on the polyimide). The SiOz layer is etched using a dry technique (to yield a anisotropic form with vertical walls) of selective exposure through a mask (photolithography). The polyimide , which is not sensitive to light, is then etched using a 'wet' process (thus isotropically) as a sub-etching, thus giving rise to the vertical 'leg' of the T. Organic layers are then evaporated, obliquely, onto the surface, as shown in Figure X-35-b , and surround the foot of the cathode separator. The metal layers are then finally evaporated perpendicularly to the substrate, schematised in Figure X-35-c, in such a way as to never touch the bases of the separators. Adjacent cathodes are thus electrically isolated from one another. While the T-form separators were prepared with dimensions of 30 11m x 30 11m [Nag 97], with present day photolithographic proce sses, dimensions as low as 10 11m x 10 11m may be reached. A passive matrix screen was prepared 256 x 64 points with pixels sized around 340 11m x 340 11m. The geometrical placement of cathodes can be rectilinear or curved, another advantage with respect to various fabrication methods.
b Integrating three RGB polymer LEDs The technology used for fabricating screens must be able to integrate sub-pixels. Polymer based orange, green and blue pixels have been prepared by sequential sampling of three polymer films on the same glass substrate covered with ITO, over which an insulating layer had been placed. The polymer films were deposited using spin-coating and then covered by a metal electrode, itself deposited by evaporation under vacuum . The last layer served as a self-alignment mask for when the films were subjected to plasma etching to expose adjacent polymer sub-layers [Wu 96]. Thus it is not the organic layer which defines the dimensions of each pixel or sub-pixel (or the LED), but rather it is the electrode (here the cathode metal or, otherwi se the ITO anode). The structure is schematised in Figure X-37 . It should be noted though that the unprotected sides of the polymer layers deposited first can be attacked by chemical agents,
X Electroluminescent organic diodes
301
Polymer
R
G
B
Figure X-37. Set-up of three sub-pixels with cathode defined.
for example the solvent of the seco nd polymer layer, which may be required for a different colour. Other than possibly forming geometrical deform ations, this process can also result in degradations and electrical short-circuits. In order to limit and even compl etely stop these problems, the structure can be modified so as to protect the side of the polymer layer. Figure X-38 shows that in order to do this, an insulating layer is depo sited onto the ITO layer, and a window which allows acce ss to the ITO layer is opened at the insulating layer, which defines the active zone. In practical terms, the insulating film is made of a nitride of silicon deposited by PECVD at 250 °C and has a thickne ss of around 100 nm. The active window is obtained in the SiN x using standard photolithographi c etching processes. For the first set of sub-pixels, the polymer film (ora nge following the particul ar reported case) is spread over the whole surface of the scree n and the cathode metal (AI included) for this layer of sub-pixels is deposited by evapora tion under vacuum (:::::: 10- 6 torr) through a mask. The structure is then exposed to oxyge n plasma which etches away resins and isolated organic materia l but leaves intact zones below the AI. This plasma etchin g is in some senses self-aligni ng and does not require a supplementary masking stage . In addition, its use negates the risks of overexposure of the organic films to solvents that would otherwi se be encountered in a 'w et' process. An additional layer of Al can be deposited throu gh a mask to seal the device, as shown in Figure X-39. Thi s takes the sides of the organic layers out of harms way from organic solvents, air and hum idity. We can also note that this techn ology can be extended to small molecules. The following green polym er layer can then be deposited to gain the second pixel. The above detailed stages, up to the sealing layer, are then repeated.
AI Polymer lnsul ling film_ (Si
',J
. -_
_
_
-tot--
l1 ~ ~
R
v
B
Figure X-38. RGB structures prepared to protect pixel edges.
Cathode metal
ITO
302
Optoelectronic s of molecules and polymers
Pnlymcr In ul tin~ film lSi, ',)
~~==--
I Carbooemct.Ill ITO
Figure X-39. Sealing sub-pixels with a layer of aluminium.
With mechanically aligned films, typicall y, dimen sions for the active zone are 2 x 2 mm 2 and the metallic contacts are 4 x 4 mm". The zones of the metallic contact go beyond that of the active material giving some space between the side of the system and the electronically useful zone. This configuration has been tested with success under a dry nitrogen atmosphere , without loss of characteristics . This technique may be extended to pixels of smaller sizes (hundred of microns ), to fabricate high-resolution screens, using classic photolithographic technol ogies. Excepting the transfer of samples from the etching chamber, all preparation steps should a priori be effected within a glove box under a dry nitrogen atmosphere. The technology described above has been used with success, and without altering optoelectronic characteristics, to prepare an integrated structure with PVK as the hole transporter, doped PVK as the emitting layers, layers of Alq3 or PBD to transport electrons and the following various dyes: PVK/Alq3/nile red for red (orange) sub-pixels; PVK /Alq3 /coumarin-6 for green sub-pixels; and PVK/PBD/coumarin-47 for the blue sub-pixels.
c Ink-jet technology [Bha 98] The techn ique of polymer spin-coating presents, in fact, a considerably number of disadvantage s with respect to preparin g pixelated screens. Normally, nearly 99% of the polymer solution is wasted and it is difficult, if not impossible, to prepare lateral faces, Deposition using ink-jets could therefore appear to be an excellent substitute method, with only less than 2% of solution lost. This technolog y also allows treatment of large surfaces, is compatible with the indispensable addressing of (coloured) pixels and is relatively cheap to operat e. Certain precautions are necessary, however, to ensure a regular deposition of polymer solution. The use of dilute polymer solutions was evaluated , with deceptive results with respect to the quality of the components. Eventually a hybrid technol ogy was adopted which uses an absorbent , intermediate layer, which can be made of a host polymer, and has a thickne ss of around 100 nm. The intermediate layer exhibit s three principal characteristics: • • •
it smoothes out bumps and dips which can be generated by the ink-jet ; it acts as a sponge, virtually fixing the polymer solution; and if it is formed of a semiconductor with a large band gap, then a multi-colour emission can be obtained by energy transfer when the ink-jet deposited material has a smaller band gap.
X Electroluminescent organicdiodes
303
In order to fabricate colour screens, red, green and blue polymers are used and the intermediate layer can be an electron injecting layer. Inversely, good results can be obtained by using the ink-jet process for the charge injecting layer and with a luminescent polymer for the intermediate layer. The emitting zone is thus defined by the charge injection layer deposited directly by the ink-jet printer. Figure X-40 shows a cross-sectional scheme of a system with the hole injection layer deposited using an ink-jet printer. A commercial printer was used with an aqueous solution ofPEDOT [bha 98]. The active polymer, MEH-PPV, was deposited using spin-coating and serves also as the absorbing, intermediate layer (120 nm thick obtained from a 1% solution of MEH-PPV spun at 2500 turns per minute). At 5 V, the 'logo sandwich' ITO/PEDOTIMEH-PPV ICa gave rise to a luminance of 200 cd m- 2 with a contrast close to 800 (the luminance ratio of emitting an dark zones) . Given the ease of controlling the ink-jet printer and its depositions, a practically infinite range of logos can be made and writing, in particular, can be computer generated. In addition to variations in colour, different grey levels can be attained by changing the superficial concentration or size of the deposited spots . Typically, plots of sizes between 180 and 400 IJ.m were possible in the original experiments. For monochrome screens, dimensions of the order of 100 IJ.m suffice. Ink-jet technology is thus well placed to be used in the fabrication of screens and this is without having to define pixel positions by overlapping lined anodes and cathodes in columns, for example. As another example, we can cite the bicolour screen [Cha 98] which was fabricated by directly spin-coating an intermediate layer onto ITO, and then ink-jet printing was used to deposit a polymer that had a lower band gap and was capable of diffusing through the intermediate layer. The intermediate layer was made from a polymer with a large band gap, was soluble in water and emitted in the blue part of the visible spectrum. The material that was ink-jet deposited was also water soluble but emitted red-orange light. On absorption, there was a transfer of energy from the former to the latter, and red-orange photoluminescence or electrolumincscence could be obtained from the ink-jet pattern, as detailed in Figure X-41. A tricolour prototype has been presented by CDT-Seiko-Epson, as shown in Figure X-42 . Its structure was based around series of pillars, formed from strips of polyimide (Figure X-42-a) deposited onto ITO and placed so as to leave spaces to receive ink-jet deposited drops of solution. After adapting the wetability of the
Cathode (Ca)
.-
.-
~ I ectroluminescent
polymer (MEH-PPV)
-Conducting polymer (PEDOT) to.node
f---
(ITO)
Substrate
Emis sion
Figure X-40. Pixel with an emittingzone defined by the charge injection layer (here, PEDOT depositedby ink-jet process.
304
Optoelectronics of molecules and polymers athode Orange polymer deposited using inkjet Diffusion of orange polymer within the layer Anode
I
EI. blue
EL urunue-red
Figure X-41. Hi-coloured pixelsobtained following excitation of a polymerby anotherwitha largergap.
polyimide by 02 and then CF4 plasma treatments, into each pixel caisson, constituted from three sub-pixels, were placed in the following order: • • • •
PEDOT by spin-coating into the base of the caisson; a red emitter and a green emitter by ink-jet printing into respective sub-pixels, as shown in Figure X-42-c; a blue emitting polymer by spin coating, as in Figure X-42-d; and a cathode (Ca then AI) as in Figure X-42-e .
6 Emerging organic-based technologies: flexible electronic 'pages' As often occurs in the course of scientific development, the electronic-ink (e-ink) technologies were developed in parallel to that of the electroluminescent (EL) organic screens. Given that most people prefer reading ink deposited on paper, it is not unimag inable to think that 'e-ink' systems will replace EL screens, at least with respect to certain needs . A group at the University of Groningen proposed the use of e-ink systems in the preparation of flexible screens , which might be used as electronic pages [ber Ola] . We could call these 'e-pages' . This technology could be adapted to the fabrication of screens operating either by transmission or by reflection, and uses as base a thick plastic film covered with micro-holes each 10 to 20 urn in diameter. The holes resemble pixels once they are filled either with a light emitter or by an e1ectrophorescing ink. For the latter, a coloured solution which contains white particulates is used. After sealing the pixels , applied electrodes can control the movement of these particles, directing them either towards the surface or the base of the plastic film and thus changing their appearance from white to coloured. The German ' start-up' company, Papyron, which developed this technology is in competition though with an American technology, developed notably by E Ink Corporation) which is based on capsules. The capsules, again between electrodes, are about 100!-tm in diameter and are filled with a dye and a white , negatively charged chip. On applying a positive tension to the upper surface electrode, a capsule appears white as the chip is attracted towards
X Electroluminescent organic diodes
305
ITO transparent anode
... .. . .. . .. . .. . .. ...
Strips of polyimidc
(a)
(b)
Red (rhodamine IOIIPPV) and green (PPV) cmiuing polymers deposited by Ink-jet
(c)
Blue emitting polymer (polydialkylfluorenc) deposited by spin-coating
(d)
Cathode deposited by evaporation under vacuum Ca then AI
(e)
Figure X-42. Steps in the real isation of a tri-colour prototype developed by CDT-Seiko-Epson.
306 Optoelectronics of molecules and polymers the screen. According to agreements made between E Ink Corporation and Philips (from the journal Opto Laser Europe, vol 5, page 84, 2001) the ink can activated using electronic controls delivered via an active matrix developed by Philips. Papyron insists that its technology exhibits numerous advantages over that of E Ink. Papyron states that its system allows a wider angle of view due to its pixels being flat rather than curving inwards and that its system allows a simpler fabrication of colour screens by filling different holes with different colours, an objective which can be realised using ink-jet technology. Thus, each pixel can be individually and electronically controlled using plastic transistors or other variants such as poly-crystalline silicon based transistors. For more stable displays, a liquid which exhibits wide variations in viscosity with changes in temperature can be used to facilitate image displays, as once the image is formed at a temperature high enough to allow easy movement of coloured particles , then the image can be 'fixed' by decreasing the temperature of the pixels, an operation which can be controlled by laser, for example . For the present time, most companies concentrate their efforts on developing systems which can be fabricated using 'roll-on-roll' techniques . A research group in Limoges, France, is currently studying the formation of micro-holes through ionic columns due to field effects, in a system probably well adapted to automatic control of the depth of micro-holes for pixel fabrication. Xerox at Pali Alto have invented a technology called Gyricon which may compete in the same domain [ber Olb]. This procedure uses a thin plastic film into which is randomly inserted small pearls. The opposite hemispheres of these pearls are oppositely charged and are black on one side and white on the other. Depending on the charge applied , the spheres present a black or white surface. A continuous application of charge is not required; the spheres do not rotate back to a certain position; their power consumption is thus relatively low. Given that this sort of technology is not sensitive to air or humidity, it can be easily transferred to large surfaces. However, the time required for each sphere to change shade is relatively long and the integration of colour (using the three primary colours) in the system is hard to envisage, so this technique may not be useful for video applications. Nevertheless, such a system is sufficiently effective to enable rechargeable electronic books, a possible market worth over US$1O billion . Other possible techniques have been evaluated, notably by Lucent which developed a polymer based 25" screen using transistors fabricated through embossing processes.
VIII The prospective and actual production at 2002 Most of the following information has come from issues of Opto Laser Europe at the end of 2001 and details the actual commercial and industrial situations at this time. The market for flat screens is worth several billions of US dollars, and concerns both e-ink technologies, which necessitate external light sources, and emitting screens based in particular on organic electroluminescence, which do not. The market estimated for the year 2000 was US$24 million, a 100% increase on 1999, while the
X Electroluminescent organic diodes 307 year 2005 is expected to encompass a market worth US$3 .3 billion . An explosion in this market is predicted for the period 2006 to 2010 . The main aims for those economically involved in this market concern the fabrication of screens which are lightweight, flexible and exhibit high luminance, contrast, wide angle of view, have low energy consumptions, and last but not least, cost little to make . The target market includes applications such as portable telephones, digital cameras, televisions - which can be hung up on walls or rolled up, tables which can act as displays, programmable and therefore rechargeable books and even wallpaper! Pioneer, with a licence from Eastman Kodak, commercialised, in September 1997, the first organic screen , which was destined for an auto-radio facade. It was based on Alq3 and had dimensions of 9.5 x 2.1 em, and consumed 0.5 W. LG-LCD in Korea announced the fabrication of a VGA screen functioning at 5 Y and displaying a contrast of 100:1. The screen was green and had a luminance of at least 200 cd m- 2 . Uniax fabricated small screens for portable telephones which emitted orange light at 610 nm, operated at 10V and required only I rnA per pixel to yield a luminance of 200 cd m- 2 . This screen was based on small molecules, much like the first colour screen introduced by Pioneer for a portable Motorola telephone. In May 2000, Sanyo Electric associated with Kodak presented an active matrix screen of 5.5" consisting of 240 x 320 pixels. The American company Universal Display Corporation (UDC) , risen from Princeton and South California universities , subsequently also developed screen s based on small molecules. On turning to technology based on polymers, a highly involved company is Cambridge Display Technologies (COT), which grew from the Cavendish Laboratory at the University of Cambridge, in which macromolecular electroluminescence was discovered. The firm Covion has announced an annual production of 40,000 litres of conjugated polymers, destined to be used by COT and by Philips, the latter having a factory in Heerlen (The Netherlands) producing screens based on light emitting polymers (LEP)s for portable telephones. In March 2000, COT and Seiko announced the realisation of a R-G-B screen based on polymers deposited using ink-jet methods . The fabrication, however, posed more problems than initially supposed, with incompatibilities arising between the polymer inks and the ink-jet deposition procedure. Collaboration with Seiko Epson brought about the presentation of a colour prototype in May 2000 and then again in May 2001 at San Jose as part of the Society for Information Display 's conference there . Lifetimes greater than 50,000 hours have been attained using adapted encapsulation procedures. COT has agreements with the Japanese firm Tokki for vapour phase physical deposition procedures and encapsulation, according OLE in July and August 200 I. A pilot line worth US$25 million was built in Godmanchester with the aim of fabricating 5 million screen units per year. The effective production was planned for the start of 2002 with 'roll-on-roll'procedures taking the place of ink-jet methods . At the University of Arizona, the ink-jet method was applied to screen fabrication and yields of 0.9% were obtained. Sony though announced the fabrication of a 13" diagonal screen with 800 x 600 pixels (SYGA), R-G-B colour and a peak luminance of 300 cd m- 2 , the device controlled by an active matrix formed from polycrystalline silicon.
!
308 Optoelectronics of molecules and polymers CDT's polymer technology has also been developed by Hewlett-Packard and Philips. The latter company has, in Heerlen, developed a pilot line for PLEDs on a glass substrate, as the flexible films were found to not entirely fulfil the role of barrier against humidity and oxygen. Philips consider that in addition to their higher luminance and wider viewing angle, organic LEDs are preferable to liquid crystal displays because of their shorter response times. By mid-2001 it was planned to realise a monochrome display for portable phones of size 65 x 100 mm and capable of displaying video images . Nevertheless, DuPont in the USA has announced a plan to develop and fabricate plastic substrates for polymer based screens on active matrixes with Philips and Alien Technology, another British 'start-up' company. DuPont have also planned, in co-ordination with other new companies, to develop more classical technologies using active matrixes on glass in China and the Philippines. The German company Osram, bought up licences from CDT and Uniax (a company started by A. Heeger and subsequently bought by DuPont) and has installed a PLED pilot line in San Jose (USA) and planned to start production in Malaysia during 2002. Japanese firms are not sitting back. Sony announced the prototype of the largest OLED screen, Toshiba planned to be selling in the market place polymer based screens by April 2002 and Tohoku-Pioneer and Sharp began an association to invest 424 million Euros into the production of organic EL screens . NEC and the Korean company Samsung, meanwhile, also formed an alliance to invest over a 5 year period 472 million Euros for the production of similar screens in South Korea from the Autumn of 200 I onwards. In England, outside of CDT, there is another relatively young company called Opsys based in Oxford which seems to be going through considerable expansion, with at the time of writing this book, 25 employees and 15 University researchers financed. The company first worked on organometallic luminescent material s, including transition metals and rare earths, and then on macromolecular materials such as dendrimers. At the same time, the company expanded in different areas, notably being the first in Europe to take up licences to exploit Kodak's small molecules . Opsys has also been developing new small molecules with greater stabilities and yields than those of Kodak, and, according to the Director, the absence of the necessary competencies within Europe have meant that they have had to go to Fremont (USA) to produce their screens. From 2002 onwards Opsys planned to fabricate their 1/1 to 5/1 diagonal screens , with active matrixes and back-lighting for portable devices. Larger screens , with appropriate licensing have been planned . The technology of the present time-based on the evaporation of small molecules-allows for little flexibility (for example with respect to changing substrate size), and it is planned that it will be changed at some point to a technology such as ink-jet or spin-coating based on polymers. The company does not see the choice between small or macro-molecules being one of chem istry or even optoelectronics, but more to do with problems associated with fabrication and costs. In addition , it seems that Opsys has already at its disposition a new class of polymers which do not fall under the umbrella of eDT's patents .
X Electroluminescent organicdiodes
309
IX Conclusion The industrial competition is wide open and the diversity of competitors currently operating is without doubt justified by the existence of such an enormous, and financially consequent, market. The market goes beyond that reached by liquid crystals and is planned to be used not only in conventional systems such as screens but also in a wide range of other devices, for example aeroplanes, cars, display panels, electronic books and in teaching systems. While the field of organic electroluminescent diodes remains young (for the most part being developed in the last 10 years), it is already vast and the number of annual publications on the subject is considerable. We can remark that a decade of intense research has actually given rise to a new source of light which is now ready to enter our everyday lives. Organic solids, largely studied during the 20th century with relatively few actual practical applications have now found in the form of electroluminescent diodes an enormous field of applications, a field which should continue to grow. In this Chapter, we have tried to present the essence of current knowledge. However, it would be highly pretentious to imagine that we have covered everything. As a useful indicator of the results of ongoing research, it is worth mentioning the reference [tro 01] which was prepared in collaboration with Thales and concerns the preparation of an OLED emitting blue-green light. A four layer structure, shown in Figure X-43 , combines a hole injection layer (HIL) made of PEDOT, an emitting hole transport layer (TNATA), a hole blocking layer (HBL) made of BCP and an electron transport layer (ETL) made of Bebq2, which has been shown to be more efficient than Alq3. These molecules and their chemical formulae are further detailed in Appendix A-II . The structure ITO /PEDOT/ TNATA/BCP/ Bebq2/ Ca, emitting in the blue-green at 508 nm gives rise to a luminance of the order of 12980 cd m- 2 operating at 11.2 V (Figure X-44). In the green though a greater luminance, more than 20,000 cd m- 2, was obtained using a tri-Iayer structure detailed in Figure X-22-b. To conclude, these results show that luminances obtainable with OLEDs can be particularly high and can satisfy the demands of a wide range of applications.
~
Cathode
v
Electron tran sport layer (ET L) Hole block ing layer ( HBL) ~---
rlt==========t: : : :;--
1 - - ' ' ' ' - - - - - - - - - - - - - ;_ _
Emitting laye r(TPD. ' PB. T ATA ) Hole inj ectio n layer (I ilL ) Anode (ITO) Glass substra te:
Figure X·43. OLEDobtained from a four layer structure.
310
Optoelectronics of molecules and polymers 12 000 Luminance (cd m· ~T
10 000
8000
2 )
'AT A
--6-
PEDOT+T . 'AT A
-
PEDOT+T. 'AT A+RCP+Alq3
-+- PEDOT+T. 'AT A+BCI' +Bcbq2
6000
Current density mAcm'!)
SOD
600
700
800
Figure X-44. L = f'(J) curves for various structure based on TNATA, including, notably, the structure ITO/PEDOT/ TNATA/ BCP/ Bebq2/ Ca.
As an example is shown the prototype screen for a portable telephone fabricated by the Briti sh firm Opsys using small organic mole cular technology, a technology in which Kodak Eastman hold s numerous patents. The screen has diagonal size of 1.24", is 1.8mm think and exhibits a luminance of 40 cd m- 2. It consists of 128 x 64 pixel s (image from Displays Europe, February 2002).
X Actual state-of-the-art and prospectives During the Society for Information Display (SID) meeting in Baltimore , USA , in May
2003, two firms claimed to have built the large st OLEOs yet. IDTech demonstrated a 50 em diagonal displa y driven by "super amorphous techn ology", a technology with a cos t much lower than this incurred with polycrystalline tran sistors. It had previously been thou ght that amorphous silico n was incapable of deli verin g sufficient current to
X Electroluminescent organic diodes
311
Figure X-45. (a): Kodak camera EasyShare LS 633; and (b) COT concept for a TV watch usingits light-emitting technology.
drive OLEO pixels, but IDTech claims that its display consumes half the power of a typical high-end LCO , and offers better colour saturation and a wider viewing angle . It has a resolution of 1280 x 768 pixels and draws 25 W of power at 300 cd m- 2 . Sony 'exhibited a substantially bigger active-matrix OLEO display at 60 em. It was comprised of four seamlessly joined pieces (displays) using a new tiling technology. The Sony display, at 1024 x 768 pixels, had a slightly lower resolution than the IOTech screen . Both companies say that their developments could lead to OLEO displays being used in televisions. Furthermore, Kodak and its manufacturing partner Sanyo showed a 15 inch OLEO screen which will be commercialised in three to four years [Ole 03-b]. The first commercialised large scale OLEO display (2.2 inch diagonal) was inserted into the Kodak Easyshare LS633 camera (Figure X-45-a) sold with a price tag of around €450. The display, with a viewing angle of 1650 has a resolution of 512 x 218 pixels and a power consumption of around 300 mW. It was developed by SK display, a joint venture between Sanyo Electric and Kodak. SK will initially produce around 100,000 two-inch OLEO displays each month , and hope to boost this value to I million at the end of 2003 [Ole 03-a1. Meanwhile, Phillips Electronics hopes to sell more than 100,000 electric shavers incorporating a small monochrome
312
Optoelectronics of molecules and polymers
OLED display in 2003. Phillips have already exhibited a 1.4 inch passive-matrix monochrome PLED at SID 2002, held in May 2002 at Boston, USA. Cambridge Display Technology (CDT) of the UK and the Japanese firm SeikoEpson developed in a joint company, Polyink, an inkjet printing technology based on light emitting polymers . They have fabricated a TV watch, shown in Figure X-45-b, and commercialisation is in progress. However, an opportunity for CDT to buy up Litrex, a Californian company which also manufactures industrial inkjet equipment, may lead to new directions being taken. It should be mentioned that displays made by Pioneer for car stereos and cell phones have been on the market for sometime already. Research into OLEDs has given-apologies for the pun-a vision of what may be possible in the future. Flexible displays could one day depict an electronic newspaper or, as curved screens , furnish the automobile or plane cockpit of tomorrow. 'Electronic ink' is an alternative way to produce soft electron ic newspaper and the E ink company of Cambridge, Massachusetts, USA, has demonstrated the world's thinnest activematrix display (0.3 mm thick) . The construction combines a thin, shatterproof steel foil transistor substrate with E ink's paper-like electronic-ink display material coated onto a plastic sheet. In 2003 the OLED display market is valued at around $500 million, and according to various market analysts (DisplaySearch, Stanford Resources, iSuppli) , may reach $3 billon (€2.7 bn) in 2007 or 2009 [OLE 03-a or Sie 03].
XI Organic photovoltaic devices
I Principles and history of organic based photovoltaics 1 General points: the photovoltaic effect a The photoelectric process In general terms, photoelectronic processes correspond to those engaged in the absorption or emission of light by a material. Solids can be subject to various effects , such as photo-conduction (conduction once the material is illuminated) or the photovoltaic effect (generation of a tension by illumination), and these effects are directly tied to transport mechanisms. Here we shall concern ourselves expressively with the second process . Within a photovoltaic system , we can see that following exposure to a ray of light, charge carriers can be generated by: • • •
electron band to band transitions (valence band to conduction band); electron transitions from localised states in the forbidden band up to the conduction band, or from the valence band to empty localised states in the band gap ; and the generation of excitons following their dissociation or their ionisation.
The first process can be found in inorganic crystalline solids, the second in inorganic amorphous solids, and the third, most commonly, in organic solids. Whatever the process though, the photovoltaic process consists of 3 steps which are: • • •
photogeneration of charges, by one of the three mechanisms above ; the separation of those charges and their transport (and eventual multiplication) to the physical limits (terminals) of the device; and the realisation of an electrically active contact that can give rise to a signal which can be analysed either as a phototension with the circuit open , or as a photo-current with the circuit closed .
314
Optoelectronics of molecules and polymers
b Various configurations used for collecting photogenerated charges For a photovoltaic devi ce to operate , the second step mentioned just abo ve is essential and can be cau sed by several different effects [Kao 8 1]:
a The volume or mass photovoltaic effect Thi s effect can arise from the diffusion of charg e carriers subject to a non- equilibrated regime, with hole s and ele ctrons each having different mobilitie s. Th is effect was first ob ser ved in 1932 in diamond, and then later in zinc sulfide, and is often called the Dember effe ct. It could be discerned at the limits of materials which were under an intense light. Submitting anthracene to light with wavelength A. = 365 nm, equ al to its fund am ent al abso rption, yields a phototen sion around 0.2 V. The negative 'pole' can be found on the side expo sed to light, as hole s have a greater mobility than electrons, and therefore the former move more readily away from the exposed side. ~ The surface photovoltaic effec t This effect appears at the interface between a metal and a semiconductor and leads to the formation of a potential barrier (a Schottky barrier as detailed in Figure XI-I ). When a metal (M) is placed in contact with a p-t ype semiconductor (SC p), and the metal has a work functi on (W M) which is less than that of the semiconductor (Wscp) i.e. Wsc e > WM, then the equilibration of Fermi levels occurs via the passage of elec trons from the met al to the semiconductor. In the semiconductor, the sa me electrons recombine with hole s and then acceptor ions (A -), negatively charg ed, are no longer stabilised by ne ighb ouring hole s. Th e result is the appearance of a negative space charge du e to a cert ain den sity (N a ) of acc eptors . Given the low value of N j , the spac e charge actually goes quite deepl y into the se mico nductor and the diffusion of electro ns from the metal to the semico nductor stops when the internal field , generated by the space charge directed fro m the met al to semico nductor, equilibrates the diffu sion curre nt. The metal takes on a positive charge near the interface and then holes there observe a barrier !:l W = x. + EG - WM, where X. and EG are the electronic affinity and the gap of the se mico nductor respectively. On the semiconductor side of the interface , hole s movin g toward s the metal ob ser ve
Vacuum level u. ed as reference
Metal
p-type semiconduc tor
Figure XI-I. Representation of the mechanisms giving rise to a phototension in a Schottky jun ction (metal/p-type semiconductor) with W SCp > W M.
XI Organic photovoltaic devices 315 the barrier Wdiff = WSCp - WM. At equilibrium, the modulu s of the current of holes going through ~ W is equal to that going through W diff - The space charge zone is not a great conductor; it is resistive due to the lattice A- ions being relatively immobile. Thus, it is also the seat of any drop or rise in tension if we negatively or positively polarise the semiconductor. If a negative tension is applied to the p-type semiconductor, the current of holes going from the semiconductor to the metal is blocked by a barrier which is raised to Wdiff + IqY-I. If a positive tension is applied to the p-type semiconductor, then the barrier is reduced to Wdiff - IqY+1 and the current of holes from the semiconductor to the metal is reinforced. In effect, we have a rectifying contact which permits the passage of strong currents going from semiconductor to metal and blocks those from metal to semiconductor. Turning now back to the photovoltaic system, there are three possible effect s in the structure of Figure XI-I , in which there is an interface between a p-type semiconductor and a metal where the workfunction of the former is greate r than that of the latter (again, Wscp > WM.): •
•
•
the absorption of light by the metal with the associated generation of a hole of energy that can overcome the barrier ~ W, only when the light is such that hv > ~ W, at the MiSe interface. With a sufficient amount ofenergy, the generated holes can penetrate into the semiconductor and form a phototension at the barrier; with an incident ray of light with hv > EG, an electron-hole pair is created in the hole depleted zone d. The intense electric field, which dominates this zone, of Eint generated on the equilibration of metal and semiconductor Fermi levels, in the direction left to the right of the Figure, efficiently separates photogenerated carriers. The result is a phototension between the metallic electrode and the semiconductor volume; and when the incident wave has a low energy, and a long wave, the optical absorption coefficient is small and in effect there is a poor formation of electron-hole pairs, as hv is not greater than EG . Such waves can penetrate quite deeply into the material and can generate, within the semiconductor volume , electron-hole pairs . In addition, minority carriers can be formed , created at a distance from the depleted zone around their diffusion length (L m ) , to diffuse towards the junction where they are controlled by the field E int . They can then contribute to the phototension at the barrier limits.
Generally speaking the first proce ss is relatively unimportant, and is associated with photoemissions with an intensity of light dependent on the thickness of the metal lic film. When hv > EG, the second and third processes are the most important. Once the photons have an energy much greater than EG, the absorption coefficient is very high and any rays are, practically speaking, absorbed near the interface. A decrease in the photoresponse is thus due to strong recombinations that occur close to the surface, where there are normally a high concentration of defaults . Photovoltaic effect s like tho se described above have been observed in anthracene [Kil 71], tetracene, chlorophyll and phthalocyanine [Gho 74]. We shall detail the photovoltaic effects revealed from these material s in the immediately following Subsection 2.
316
Optoelectronics of molecules and polymers
y The photovoltaic effect produced by an internal field at a hetero- or pn junction As in the case above , the internal electric field across a space charge zone propels in opposite directions the photogenerated charge carriers, resulting in the formation of a phototension. There are now standard texts which well detail the theories associated with devices , essentially made from inorganics, based on these effects (photovoltaic cells) such as Section 9.2.4 of [Mat 98]. In organic materials, most photovoltaic effects are obtained using Schottky pn-junctions, which require two types of semiconductivity. In Section 2 we will cite the example of phthalocyaninejperylene. Here the former component, p-type, is a highly coloured chemical, historically derived from the conversion of disubstituted ben zene derivatives . The second, n-type, is a polycyclic hydrocarbon with the chemical formula C20H12 and is used in the preparation of dyes. To give an overview, the development of solar photovoltaic systems has up until now been essentially shouldered on inorganic semiconductors, in particular polycrystalline silicon. While the maximum yields approach 24%, the cost of fabrication of the raw materials have limited commercial developments. Alternatives using microcrystalline or amorphous silicon have been widely studied and maximum yields have neared 15%. Nevertheless costs remain a problem due to processes based on the use of highly polluting materials, leaving them to compete poorly with other energy sources. In parallel, the use of organic semiconductors, developed during the 1970s and 80s [Sim 85] was also envisaged as a possible route . In the following Sub-sections 2 to 4 we will show the more notable results, before going on in Section II to describe rr-conjugated polymers and organic systems based on specific structures under going development at the present time, notable interpenetrating materials.
2 Initial attempts using organic materials: the phthalocyanines While the first results were hardly very encouraging, with yields of the order of 10- 2 to 10-3 %, significant results, around 1%, were realised in 1978 using merocyanine [Mor 78] . The considerable problem of instability associated with organics put considerable break on their development. This was in part resolved though by using phthalocyanines (Pc) . Indeed, this material has found commercial success as a photoconductor in photocopiers or printers (Xerography). Their chemical structure, shown with the example ofCuPc in FigureXI-2, is close to that of chlorophyll [Keo 98], indicating that real possibilities do exist for the conversion of solar energy. Two clas sical configurations have been explored with this material: Schottky and pn-junctions. In both cases, the Pc layer on being submitted to light rays is used to generate electronhole pairs . Their separation by an internal tension, which governs the limits of the junction, can give rise to a photocurrent in an external circuit. As shown in Figure XI-3, the Schottky junction is typically prepared with a sandwich structure. The p-type semiconductor, phthalocyanine (see also Chapter X, Section IV-I-a), is placed between an electrode that ensures an ohmic contact (Au or ITO , which have high work functions) and a second, rectifying electrode which permits the passage of current from the p-type semiconductor towards the latter metal (AI or In, which have low work functions) .
XI Organic photovoltaic devices
317
Figure XI-2. Structure of the CuPc molecule. IT O or Au
Pc
Figure XI-3. Configuration, under light, of a Schottky PclAl or In j unction.
The rectifying effect, detailed in Figure XI-4, can only be efficient if the phthalocyanine layer exhibits a negative space charge and is truly p-type. If the layer is deposited under air it shows strong rectifying properties (Figure XI-4-a), however, if deposited under vacuum the same properties are only weakly exhibited
I I I
I
- - --
~
v
(at
Under light (c) _ . /
.-
.
'
Figure XI-4. The (a) rectifying or (b) non-rectifyi ng behaviour with respect to deposition conditions used with CuPc; and (c) the resulting J(V) curve obtained on exposure to light.
3 I8
Optoelectronic s of molecule s and polymers
(Figure XI-4-b) . In general, the degree of contamination by oxygen is highly variable, making it difficult to compare result s from different laboratories. However, the characteristic curve obt ained under light, as in Figure XI-4- c, can be used to determine the open circuit tension (Vco) (the photovoltaic regime) and the short circuit curre nt (l ee) . The maximum electrical power (P maxJ is such that P max = Vmax Jmax = Jcc Vco F. The factor F, called the fill factor , dep end s on the series resistance of the device. Vmax and J max are defined in Figure XI-4. The yield of the system, generally expressed as a percentage, is the ratio of maximum electrical power to the power of the total incident light. Using this Schottky configuration , yields of I% were finally attained using materials based on a spacer group (X) and non-metallic phth aloc yanines (X-HzPc) and lighting through an indium electrode. The poor tran sparency of the electrode resulted in a global efficiency of only 0.2 to 0.3%. Lighting the device from the side of the tran sparent electrode (ITO ) did not improve the result due to the Pc layer filtering light, which otherwise would have reached the space charge zone situated near the indium electrode. The use of pn-junctions should, in part, help overcome the problem associated with absorption due to the metallic electrode, used as a rectify ing contact. This is because the space charge now appe ars at the interface betw een the Fl- and p-type semico nductors. Structures based on n-type perylene and p-type Pc, schematised in Figure XI-5 , have been experimented with. Better perform ances than those observed with Schottky structures were obtained, due to a higher degree of light tran smission to the space charge zone. Exciton s which diffused up to the inte rface between the two semiconductors were thu s ionised and the electrons and holes could be coIIected. With devices sufficiently thin , a fill factor of 0.65 can be obtained. Tang, using this meth od [tan 86], reali sed conversions of the order of 0.4 to I%. However, a higher value is required for the sys tem to be viable at an indu strial level.
3 Solar cells based on pentacene doped with iodine [ScM OOb] In order to dope pentacene with iodine, the pentacene is introduced into a hexane or acetonitrile solution of iodine and left there for 72 h. Thi s proce ss gives rise
Figure XI-So Organic pn-jun ction under light.
XI Organic photovoltaic devices
319
to a good p-type semiconductor. The iodine molecules are incorporated between layers of pentacene molecules and the resulting charge concentration can vary from 107 to 1018 cm- 3 . The iodine enables a high charge mobility (comparable to naphthalene and anthracene at 1 to 2cm 2 V-I s-I) and good electrical conductivity, in addition to the efficient separation of charges. Useful also is the displacement of the absorption spectrum (threshold at 1.4eV) towards that of the solar spectrum. The increase over several orders of size of the quantum yield of this system, which can reach from 1.9 to 2.4%, can be reasoned by the following mechanism: • •
the incident photon is absorbed by the active zone where an exciton is formed (Figure XI-6~a); the exciton diffuses into the neighbourhood of an iodine dopant molecule to generate an excited state at the pentacene-iodine-pentacene complex level (Figure XI-6-b);
000000 000000 000000 000000
000000 000000 000000 000000
::~O~:
OOi~/)OO
~
OOOO
() 7)000 u. o 0000 000 000000
000000 OOOOr 00000 00000
0 0:0r;,g0
~
o 0000 o 0000 o 000
000000 4 --
(a)
000 00 000 '-f}0 000 00 000000
(b)
000000 o0fIJO (). 000 000 000 0 000 0
(d)
(e)
OO~OO
000 00 000 '-f}0 000 00 000000
-\0:
Figure XI-6. Charge photogeneration in the pentacene-iodine system: (a) photogeneration of an exciton; (b) diffusion ofthe exciton near to the iodine ; (c) transfer of negative charge towards the iodine and dissociation of the exciton ; and (d) separation of positive and negative charges under the field (E) effect.
320 Optoelectronics of molecules and polymers • •
the negative charge of the exciton is partially transferred towards the doping molecule (Figure XI-6-c) and thus aids in the dissociation of the exciton; and the hole and electron are finally separated and the charges carriers are collected, with the help of an electric field, to yield the photocurrent. (The electric field which gives rise to the collection of these charges is an internal field generated by a Schottky junction or a heterojunction).
The lifetimes of such devices remain controversial and it is for this reason that any results announced should be viewed with some caution. Cells with dimensions 5 by 5 mm have been made using the structure ITO/iodine doped pentacene (50!tm thickj /Mg or Al and have yielded Yeo = 995 mY, lee = 4.5 rnA cm- 2 , and a fill factor (ff) of 0.45 .
4 The general principle of Graetzel and current organic solar cells In general terms , and as we have already seen in some examples, the heart of a solar cell consists of a semiconductor which normally absorbs photons and thus passes electrons from valence to conduction band s. This requires that the photons have at least a minimum energy and that excess energy is lost, even if this means that in the best materials 50% of the available energy is wasted. It is for this reason that the size of the forbidden band (Ea) must be well adapted to the incident light. Excess photon energy, with respect to Ea, results in the thermal excitation of photoelectrons towards the LUMO band minimum (with, for example, an excitation of lattice vibration energy). In the natural world, green plants which use solar energy are apriori subject to the same problem. Graetzel [Gra 91 J was inspired to transfer the solution that they provided to photovoltaic system s. In plants , light is recovered by chlorophyll molecules which exhibit an absorption band well adapted to the solar emission spectrum. In effect, few photons are not used. Once the solar energy is absorbed, it is transferred via a protein complex in which a separation of charges gives rise to chemical reactions. These reactions convert carbon dioxide and water into hydrocarbons and oxygen . In terms of photovoltaic systems , the principal idea applied during the I970s came from the same logic. In order to limit losses, the processes of light absorption and conversion to electrons were separated. Initially therefore, the structures were based on a layer of absorbent dye molecules deposited on a SC surface . Once the dye molecules were excited, they liberated, or rather transferred, an electron to the SC conduction band . This completely removed the dependence of photon absorption with respect to the SC absorption spectrum. The problems that are now faced are : • •
the efficiency of electron-hole pair (exciton) disassociation; and the efficiency of charge transfer towards the SC and the following collection of charges at the electrodes.
In practical terms, the slow transfer of charges from the dye required that this layer be extremely thin. If not, numerous recombinations could occur. The available material
XI Organic photovoltaic devices
321
for absorption is thus reduced and the numb er of electrons that can be generated becomes limited. So, rather than using a specifically semico nducting material, such as crystalline Ti02, Graet zel prep ared a porous material from a large number of colloidal Ti02 particles and impreg nated it with dye molecules . The particles, whic h were hardly 20 nm across, were in effect inserted within a dye layer of about I micron . The effec tive spec ific surface area of the dye using this technique hence became very large indeed. Now standardised, the Graetzel cell is made up of a liquid electro lyte sandwiched between two transparent electrodes.The instability ofthe system, due to evaporation of the electrolyte, however, does demand a low operating temperatu re range, something which has tended to limit their wides pread use. Poly(para-phenylene vinylene) (PPY) and its derivatives are, at present , materials widel y under investigation for insertion in porous Ti02 matrices. A problem remain s in the macromolecular size of the PPYs, especiall y important now that the Ti02 is prepared on a rotating disc from a very fine powder. At the Universities in Santa Barbara and Cambridge, principally, research has now centred on the use of buckm inster fullerene (C60) in place of Ti02 in composites with PPY. Here a PPY chain is grafted onto C60, and we will look at these materials now in more depth .
II n-Conjugated materials under development for the conversion of solar energy There are many envisaged advantages to maki ng polymer ('plastic ') based photovoltaic systems. They includ e their ease of fabrication and manipulation, their flexibility and low weight and their low cost, all of which are good reasons to imagine their facile integrati on into buildings. These expec tations have done much to push research rapidl y forward over the last few years.
1 Metal-Insulator-Metal structures On using the structure of organic LEDs as a basis, the classic metal-insulat or-metal (MIM) structure was envisaged as a possible route to the preparation of photodetectors. Organic LED s were , incidentally, the first optoelectronic devices made using n-conjugated polymers. As shown in Figure XI-7, once a cont act is made , then the alignment of Fermi levels adju sts band positions. Without an applied tension, i.e. Y = 0, there is a swing in the polymer bands so that, still without the application of the external field , there appears an external field Eint = - grad Yint =1= O. The difference in intern al potential is due to the energy differen ce D. Wint = Wanode - Wcathode, i.e. the difference in work functions of the anode and cathode metals. With the inception of a photon an exci ton is produ ced. Under the photovoltaic regime, only the slight difference in internal potenti al controls-with a low yieldthe dissociation of the photogenerated quasi-particle. In practical terms, the generated phototension is not great enough to be of any use. With the struct ure ITO/ PPY ( 120 nm
322
Optoelectronic s of molecules and polymers
WlUlOd<
Figure XI-7. Photogeneration of charges in a MIM structure.
thick j/Mg, the tension at open circuit is 1.2 V and the short-circuit current is equivalent to a quantum yield of I% (electrons collected per incident photon). This yield, however, improves drastically once the system is subject to an inverse polari sation (around IOV) and can permits envisaging this system applicable as a large surface photodetector. The use of a Schottky structure resulted in only a slight improvement in charge photogeneration. It is generally acknowledged [Mar 94] that charge photogeneration in the volume of the material occurs through dissociation of exciton singlets under field effect s. Instead of traver sing the polymer layer, electrons are either trapped or undergo combination with hole s, giving rise to an rather unremarkable result.
2 How bilayer hetero-structures work and their limits Following on from the fund ament al principles, deri ved from the photo synthetic systems described in Section I, any impro vements in the photoph ysics of the precedin g organic monola yer structures (MIM or Schottky M-SC) necessitate the use of bilayer systems. The use of a donor/ acceptor structure would allow the efficient transfer of photo-electrons from a 'donor' semiconductor n-conjugated polymer (p-type semiconductor POD ) toward s an ' acceptor' material which can either be an n-type rr-conjugated polymer (which are rather rare ), or an accepting molecule, of which the archetype is C60 .
a Production and collection of photoinduced charges The making and harve sting of photoinduced charges follow s the proce sses given below: • •
the incident light generates electron-hole pairs at the p-type donor polymer (POD) due to electron transition s from n HOMO to rr" LUMO band s; the created pair is separated close to the acceptor, and electron s generated in the POD LUMO band are accepted on energetically favourable term s into the acceptor LUMO band. As Figures XI-8 (which shows the flat band co ndition) and XI-IO
XI Organic photovoItaic devices (b)
(a)
1t*MEH-PPV
-LUMOC .............
2.8 1t*MEH-PPV LUMO-C~
..............EF
3.7
323
0
.
4.3 Al 4.7
1tMEH-PP
ITO
5 1tMEH-PPV HONIOL60- .1
--
- Eint +
Figure XI-S. (a) Flat band regime of MEH-PPY jC60 system; (b) Energy levels in the MEHPPYjC60 system in the shortcircuitstate.
•
indicates , this is due to the acceptor LUMO being of a lower energy than that of the POD LUMO ; the separated charges are propelled in opposing directions due to the internal field-to be collected-and as schematised in Figure XI-8-b.
b Transport of photoinduced charges to the electrodes In order to transport charges up to the electrodes, the photovoltaic system exploits the relative conductivities of holes and electrons with respect to the constituent donor and acceptor molecules in the composite. a Transport in the p-type donor polymer Once the donor p-type rr-conjugated semiconductor polymer (POD) is excited by incident light, the first process it undergoes is the transfer of electrons from the bonding rt-orbital to the antibonding rt" -orbital. Once the excited electron is transferred to an acceptor molecule, in this example C60, then a polaronic state, associated with a positive polaron , appears on the POD chain. What we are observing here, in a sense, is a localised photodoping. The polarons have transport mechanisms detailed in Chapter IV. ~ Transport in the n-type acceptor C60 Once an electron is transferred to the C60 from the POD, it can benefit from the n-type semiconductor character which C60 exhibits to be transported throughout the C60 phase. Chapter III gives more relevant details .
y Overall result The rapid transfer of a photoinduced electron from POD to C60 permits reinforcement of the generated charges at POD and assures the separation of photogenerated charges-by enhancing their stability through a polaronic effect. It is thus possible to obtain a heterojunction with a rectification factor of the order of 104 for a bilayer structure based on poly(2-methoxy-5(2'-ethyl-hexyloxy)p-phenylenevinylene) (MEH-PPV) and C60, as schematised in Figure XI-8-b. In addition to which, it is possible to yield either a photocurrent or a photovoItage .
324
Optoelectronics of molecules and polymers
c Properties and practical limits of donor-acceptor bilayer systems The photophysics of bilayer systems have been studied in depth by C.J . Brabec and N.S. Saricifti [bra Ola] . Notably, it was shown that the time required for a decrease in the luminescence of MEH-PPV (1: = 550 s) was reduced by more than one order by the presence of C60 . Thi s 'quenching' of luminescence by C 60 seems to be a general phenomena for all rr-conju gated non-de generate polymers. In particul ar, it indicates that the transfer of a photoinduced electron occurs during an interval sufficiently short to limit any radiative relaxations of the excited, conjugated polymer. However, a bilayer system must present some limit s in performance, as even though the system has a high optical absorption coefficient (~ 1 05 cm""), the absorption zone is considerably greater than the exciton diffu sion length. As the exciton can only dissociate in a volume close to its zone of existence (the region at the interface between the donor polymer and the C60 and no further from the C60 than the short exciton diffusion length), all photoexcitations generated outside of this zone are condemned to undergo recombinations without generating efficiently separated photo-carriers. They cannot, for example, participate in the form ation of a photocurrent. Also, the photovoltaic effect arises only from photons absorbed with this thin layer. An improvement in this situation can be made by introducing layers with high levels of optical absorptions or, alternatively, by using crystalline semiconductors of a high level of purity which allow longer exciton diffusion lengths. Another approach to impr oving this system involves using elaborate thin films constituted of intimate mixture s of both the conjugated polymer and C 60. There is thus a large surface area for absorpti on which is alwa ys clo se to a POD and C 60 interface , where the dissociation of an exciton can be assured [Hut 011. Figure XI-9
------------------------ r-
11 :;
0
r c--
,........... t'!l
l<
e.
0 Q
:l
., Q
N Q
"Cl
:l
::r
'-
J
~
'"
'--
S'
:l
e,
'" ~ o· :l
'--
"Cl
-
"Cl
'" ::
> n n
'"
S' ., ::r
e1
o ~
::r
8-
'--
'"
-
(a)
(b)
Figure XI-9. Schematisation of (a) a bilayer structure; and (b) an interpenetrating structure.
XI Organic photovoltaic devices
325
gives two repre sentations corresponding to a classic bilayer device (Figure XI-9-a) and a device made using a compo site of two interpenetrating phases (Figure XI-9-b ).
3 Volume heterojunctions a Principle At each donor-accept or element constituting the composite, the same mechanism is reprodu ced. That is, the creation of the exciton, its disassociation and the transfer of an electron from the donor to the acceptor, and the eventual separation- in opposite directions-i-of the hole in the donor phase and the electron in the acceptor phase under the influence of the internal field generated by the asymmetric electrode s. This process is detailed Figure XI- IO. As the zone of interaction betwe en the donor and the acceptor are not reduced to a simple plane (as found in the bilayer system in Figure XI-9-a), these compo site devices present a zone for the absorption of light which is sufficiently thick while at the same time maintaining the process of dissociation and separation of charge carriers in the volume of the layer. Outside of this , the transport mechanisms are the same as those exhibited by the bilayer device, and the mechanism used in the physical transfer of charges is the same as that schematised in Figure XI- I I. It is for these reasons that an interpenetrating composite can exhibit high (close to 100%) efficiencies in charge generation. It can be thought of as interpenetrating latticework of donor/ acceptor heterojunction s, allowing efficient separation of photogenerated charges throughout its volume via the two n- and p-type phases. In effect, the photoactive layer is one mass heterojunction. The two intermixed material s of different gaps give rise to zones of sub-systems with levels where electrons are transferred between donors and acce ptors. The ideal situation is that the acce ptor is placed at a distance less that the diffusion length of the exciton so that the separat ion of the photogenerated pair, or in other term s the dissociation of the exciton, is facilitated.
b The results Under solar light, efficiencies have reached 3% [Brab Ola]. The composition and morphology of the film is, however, a critical factor. Rather than obtaining composites which are completely homo geneous, the films are rather disorgan ised, with isles form ing of each component material. The size of these aggregates depends on the solvent used to prepare the film. As an example we can site the use of chlorobenzene and toluen e, the former giving rise to smaller aggregations. Th is effect acts directl y upon the performanc es of the device as the smaller the size of the aggregates, the greater the specific interface zone available for dissociation of excitons. We should also remember that the donor-accept or matrices should interpen etrate to a sufficient degree, so that the transport of the two charge carriers is assured. A high concentration of C 60 can increase both the yield of photo-carriers and their lifetime s, resulting in a global increase in photo-current.
HOMO
Donors
eo
_
I .
.....
Donor
L UMO ___.
1I0MO
HOMO
L UMO
e e ti31:
- en '" :: C :"
i:~
Excited donor
'-"
.....
•
--
c ..
1I0MO
Accep tor
':xcit:ttioll
LUMO
HOMO
Donor+
e-e
L UMO - - - -
re laxat ion
---I--
i
C'
'-'
__
Acceptor-
Dnnor'"
-
-
-
-
-----:.i---
HOMO
HOMO
LUMO
I
Figure XI-IO. Schematisation of: (a) the formation of an exciton at an irradiated donor; and (b) transfer of an electron from an excited donor to an acceptor. In effect, a hole or electron carrier are formed , respectively, from the donor and from the acceptor.
EJI
I
B
LUl\1O
tv
W
'"
« ~
o
'0
::l 0-
'" t.:>
o 0" n s:: 0"
3
'" o ....,
::l
"'.
g
[
~
o
0\
XI Organic photovoltaic devices
~ o
n-conjugated polymer chain (POD)
Cathode AI
327
e
Cw Charges arc photo-generated Photo-induced electrons and transported
Positive polarons transported along POD.
Figure XI-H. Schematisation of the physical processwithin a composite of POD and C60.
Outside of the system based on MEH-PPV/ C60, the research teams of A. Heeger at Santa Barbara [Yu 95] and R.H. Friend at Cambridge [Hal 95] successfully experimented, independently, with a composite based entirely on polymers. The system used was based on MEH-PPV and CN-PPV, the former acting as the donor and the latter, a cyanide derivative of MEH-PPV, acting as the acceptor. CN-PPV exhibits a high electron affinity due to the presence of -C == N groups substituted on its backbone (which have a character discussed and detailed, respectively, in Chapter X, Section IV-I-c and Appendix 1-10). As shown in Figure XI-8-a , and much like C60, the LUMO of CN-PPV is below that of MEH-PPV. More recent studies have resulted in even higher efficiencies by gradating the stoichiometries of the different components in the layers, facilitating conduction of electrons and holes in the volume of the heterojunction [Bra Olb] . c Using n-conjugated polymers grafted onto C60 One way of reinforcing the contact between donor and acceptor molecules, and overcoming phase separation, is to directly graft the donor chain directly onto the acceptor. Thus , a bicontinuous medium is obtained. There are two notable examples: • •
grafting poly(para-phenylene) onto C60 (a route chosen by E. Mignard et at) [Mig 01]; and grafting oligo(para-phenylene vinylene) (OPV) onto C60 [Nie 99].
Using the structure ITO/C60-0PV/Al allowed both the generation of electrons and holes and also their collection at opposing electrodes. On exposure to light , using the oligomer tri(para-phenylene vinylene) (3PV) an open circuit tension of 0.46 V was obtained, roughly equivalent to the difference in work functions of the ITO and AI. Under short-circuit conditions, the photo-current was found to be 10 I!A cm- 2 and the fill factor 0.3. The rather poor yield, nevertheless more than two orders greater than that of a layer of 3PV alone without the C60, could be explained by considering that the transfer of photoinduced electrons (Figure XI-12, level I) between the 3PV and C60
328
Optoelectronics of molecules and polymers C60-\3PV)
_0#----.. . . . . . --
+
(C60H3PV) ~ ---I I
I
!
II
1(C60)-3PV
I I I
hv
I
! I I
3(C60)-3PV
.....L._ _""""'-'L-
C6o-3PV
-'-_-:fc::.un::;-damental level
Figure XI-12. Schematisation of theenergylevelsinvolved in the relaxation of C60-3PV (after I.E Nierengarten, G. Hadziioannou, MaterialsToday, 4, (200I), 16).
Coo-4PV
Figure XI-13. Representation of the compound C60-4PV.
molecules was in competition with an energy transfer to the lowest energy singlet state of C60 (Figure XI-12, level II). A better result was obtained using 4PV in the structure shown in Figure XI-B, indicating the relationship between structures and characteristics. These results do highlight the route towards other developments based on, for example, new derivatives of C60 [Nie 0 I].
III Additional informations about photovoltaic cells and organic components 1 Discussion about mechanisms leading to the generation of charge carriers in organics The making and harvesting of photoinduced charges follows the processes given below where donor and acceptor materials exhibit an interface which induces charge separation. Figure XI-14 details the various processes of varying efficiencies (11), which are: (1) photon absorption (l1A) . The incident light generates electron-hole pairs at the p-type donor material (POD) due to electron transitions from n HOMO to n" LUMO bands . llA depends on the value of the optical absorption coefficient and on the thickness of the donor material;
XI Organic photovoltaic devices 329
Anode (6},
iJ
I
'\. , 0 " \. - "(J) »TJ'; -; , O~ nee '0 ,HOMO I
;:.
I
\.
I
\.
Figure XI·14. Mechanisms of photocarriergeneration in organics.
(2) generation of excitons.The generation of an electron-hole pair, by photoexcitation, results in an excited but neutral state with a limited, finite lifetime. This state is termed an exciton and consists of an electron and a hole paired by excited energy states (Eex) within the limits of permitted bands (LUMO and HOMO bands, respectively) . The occupation of these excited states , the LUMO by the electron, the HOMO by the hole , is termed a non-recombined exciton generally observed in organic materials; (3) exciton diffusion (lldiff). This quasi-particle diffuses inside the donor material as long as recombination processes (of the hole-electron pair which make up the exciton) do not take place. The Forster (long range) or Dexter (between adjacent molecules) transfers can take place between an excited molecule (considered as excitation donor) and a molecule that receives the excitation (excitation acceptor) . TJdiff < I because various recombinations can occur in the thick donor material ; (4) hole - electron separation (exciton dissociation) (nrc). If the diffusion length is sufficiently long so that the exciton meets an internal field, hole and electron separation occurs. The internal field may be obtained at a donor-acceptor interface, provided the LUMO level of the acceptor is lower than the excitonic state located at the bottom of the conduction band of the donor. More precisely, Figure XI-14 indicated that the condition which must be fulfilled is Eex > Ipd - XEa, where Eex is the bounding energy of the exciton, Ipd is the ionisation energy of the acceptor, and XEa is the electronic affinity of the acceptor. As this condition is generally verified, nrc ;::;; 1; (5) carrier transport towards the electrodes (lltr). Thi s transport involves the classic mechanism for hopping proce sses in organic materials. Traps can reduce the mobility. If carriers are not infinitely trapped (as for example in lattice defects such as dislocations), we can consider that lltr = I; and (6) charge collection at the respective electrodes (nee) - For this to occur, (EF)eathode < (ELUMO)aeeeptor and (EF)anode > (EHOMO)donor. When fulfilled, nee ;::;; I.
330
Optoelectronics of molecules and polymers
2 Electric circuit based on an irradiated pn-junction; photovoltaic parameters For this study, we will consider a pn-junctionwith an ohmic metallic contact.
a Current inside the junction under short-circuit conditions and in the dark The Fermi levelsare alignedon the samehorizontal line and thebarrierwhichprevents the major carrier flowing is qVbO = WsP - WsN, where WsP and WsN are the work functions of the p- and n-type semiconductors (Figure XI-IS-a). If we denote with the index 0 the currents in the dark, the resulting electron and hole currents are, respectively: JOn = l onN JOnP _= 0 (~oduli of the majority and minority electron currents are equal); and jop = Jopp + jOpN = 0 (moduliof the majorityand minorityhole currents are equal).
±
(a)
-
J""
h laj
P -
(c) qV ~M
M,
E. -_J__________________________ E,.~ _ ----'--.L..J qV oc - = q(V
-
Vb)
bO
-_---J z~
}-
-
Figure XI-IS. Current densities in a pn-junct ion (a) under short-circuit condition s and in the dark; (b) under short-circuit conditions and under irradiation; and (c) in open circuit and under irradiation .
XI Organic photovoltaic devices
331
The resulting current is of course zero: Io = Ion + Iop = 0, and we can write: Io = cJOnN + l opp ) + UOnP + IOpN) = l Maj + Is, with (10nN + l opp) = l Maj (current of majority carriers) and UOnP +IOpN) = Is (saturation current).
b Current inside junction in short-circuit and under irradiation Under short-circuit conditions, the Fermi levels remain aligned, but in the irradiated areas the ~ermi le~el s b~come £he qua~i Fermi levels as shown in Figure XI-15-b. We then have JMaj = JnN + JpP :::::: JOnN + Jopp because the irradiation does not drastically modify the density of the majority carriers. Conversely though, the minority carrier densities are strongly modified in the n- and p-regions because of the irradiation which generates the hole-electron pairs. The minority electron and hole currents are thus jnP » jonP and jpN » jOpNand the resulting current is practically generated only by minority carriers as in Is = InP +IpN. Inside the space charge area there is some recombination of electrons and holes to give a recombination current which we will neglect. In addition, hole-electron pairs are also generated in the space charge area and giving a current going from the n to the p region which is denoted JGen in Figure 24-b. As a result, the irradiation Erodu: es a reverse current (going from the n to the p zone) and we can write: lph = jsat
+ JGen·
c Junction in open-circuit and under irradiation (Figure XI· IS-c) This situation can be obtained when the junction is connected to an electrometer/vo ltmeter of high impedance (Zelectrometer ~ 00) . The Fermi levels move closer to one another as the metallic electrodes are not directly connected by means of a short-circuit and a voltage appears across electrodes. Becau~e the : ircuit i: open, the current density is zero and 1 = l Maj + Isat + l Gen = 0, where jsat + JGen = Jph is the same reverse current as that calculated above in §IV,2,b. l.:,he resul~ng cu_rrent bei~ g zero, the majority current must now be increased so that IJMaj I = Usat + JGenI = IJph I· In fact, if the majority current is increased, then that means that the barrier which prevented the flow of the majority carriers is reduced from its initial value of qVbOto qVb, which verifies qVb < qVbO. So that the barrier observed by majority carriers becomes qv j, (for example, barrier to electrons on the metal (M2) side), the Fermi level must be raised on the same side by a value qVbo - qVb = qVOC, and thus Voc = VbO - Vb is the voltage which appears at the contacts in the open-circuit configuration. The n region which is initially positive with respect to the p region with a value VbO, becomes less positive under irradiation (with a value Vb < VbO). What is important is to underline that, contrary to what is often stated, the voltage in an open, irradiated circuit is not equal to the voltage difference between the surfaces
332
Optoelectronics of molecules and polymers
of nand p regions and (Wsp - WsN)/q = VbO. This value is the bias voltage which has given, not without some error, the name photovoltaic. As demonstrated above, the value for Voc is given by the variation in the potential bias between its value without and with irradiation and it is only when Vb -+ 0 that we have Voc ~ VbO. VbO = (Wsp - WsN)/q is thus the maximum value that can be reached by Voc. the open-circuit voltage for an irradiated pn-junction.
d Electrical characteristics If the non-irradiated junction is biased with a voltage V, the current of the minority carriers is unchanged at Js- while the majority current is exponentionally reinforced to become JMaj
= is exp (~~) . The resulting current density is thus:
When the junction is irradiated, the current density becomes:
(1)
and we have the characteristics shown in Figure 25-a . Under irradi ation , the curve no longer goes through the origin. The irradiated biased junction can thus work as: -
a rectifier with a forward bias V > Voc in the first quadrant;
-
a photodiode with a reverse bias in the yd quadrant where V
«
+ Jph) that is to say with js Jph, J ~ -Jph. The measured current is approximately proportional to the irradiation and when V -+ 0, I -+ Icc ~ - Iph (short-circuit current); and a photovoltaic cell without external bias, but with a current flowing through a load resistance RL in the 4th quadrant so that the photovoltaic function is not reduced to the open circuit only. In this 4th quadrant, the product of VI is negative so that power (and electrical energy) can be produced by the device . With I' = -I, the curve I' (V) can be depicted for the general case in the first quadrant (see Figure XI-16-b) where the optimised (maximum) power (P max) fits the values I' = I:n and V = V m so that P max = Vml m. J = -(js
-
kT « 0 and IV I » -, q
The fill factor (FF) is then defined as the ratio of P max to Voc x Icc and can be P max
written FF = - - - Voc x Icc
XI Organic photovoltaicdevices 333
(b)
(a)
J
l'
1ICClr_ I;" .-: ~·-.-: ~·-.-; ~·-.-; ~I · Ma~i!Jl)J~ : .:
: l:io~~r: .:.:.:~
------:-l-==--+--+V
·rectangle .:' } •• •• •••••••. ••.L ·
.
.•
.
..
-I
v; Voe ee =-
ph
Figure XI-16. (a) J(V) characteristics; and (b) I' (V) characteristics with the maximum power rectangle.
Furthermore, the open-circuit voltage (Vod can be directly deduced from relation (1), where J =0, so that we have:
kT Voe=-Log q
(J
ph kT (Iph -+1 ) = -Log -+1 ) . Js
Is
q
(2)
e PhotovoItaic parameters The internal quantum efficiency (IQE) , is defined by IQE = Jldiff x T]Te x T]tr x nee . while the external quantum efficiency (EQE), is given by EQE = T]A x IQE . In effect, the EQE, obtained by the multiplication of all the efficiencies, represents the ratio between the number of generated electrons to the number of incident photons. This coefficient, also named the Incident Photon-to-Current Efficiency (lPCE) represents the ratio between: -
-
the measured photo current ex~ressed as the number of collected electrons in the where Icc = Icc/S is the current den sity unit time and per unit area: lc~ S = in A cm - 2 ; to the intensity of the incoming mon ochromatic light expre ssed as the number of incoming photons (of "'- wavelength) per unit time and area : ~~j~ = ~; cPe is the incident energetic flux (expre ssed in Watt) and E, is the illumination defined by E, = cPe/S (in W / cm 2 ) . Thu s, we have:
¥,
EQE = Icc x hc = Jee x hc .
cPe
e"'-
Ee
e),
With "'- expressed in urn , numerically, EQE = 1.24 {;~e . Finall y, the external power conversion efficiency T] is defined as the ratio of the maximum electric power P max to the energetic flux cPe = E, x S i.e.T] = = XVoc. This yield is the maximum value for the theoretical yield , and to optimi se FFxlc;e
P;:,
this yield we have to optimise each of the three factors in the numerator. In practice,
334
Optoelectronics of molecules and polymers
the yield is diminished by two factors: the effect of the serie s and shunt resistance s and the effect of reflection at the surface of the cell.
3 Circuit equivalent to a solar cell a Equivalent circuit for an ideal solar cell As I = Is [exp
(~~)
- I] - Iph, the biased and irradiated pn-junction can be seen as
a current source Iph (a reverse current proportional to the incident light) in parallel with a diode in the dark which delivers the current i = Is [exp ( ~~) -I]. We thus obtain the equivalent circuit for an ideal solar cell, outlined in Figure XI-17, which consists of an ideal diode and a current source in parallel. If the junction is connected to a load resistance (Rd , the voltage (V) is the result of the ohmic fall of the current through RL (in open circuit, RL -+ 00 and V -+ Voc). The orientation of Iph towards RL produce s a V which induce s a forward bias across the junction so that the current (i) is a forward current in the direction opposite to Iph . Altern atively, we can consider that the direction of the photocurrent in the load resistance induce s a voltage across the j unction which generates the i forward current in the direction opposite to Iph , so that in the external circuit we do not observe the entire Iph photocurrent, but only I' = Iph - i.
b Equivalent circuit for a real solar cell When the contact resistances (electrode resistivity and metal-materials interfaces) and the ohmic losses (due to the bulk resistivity ofthe material s) generate a non-negligible resistance in relation to the load resistance , we must include in the equivalent circuit a series resistance (rs), as detailed in Figure XI-18. If we denote Vj the voltage across the junction, the voltage V across the cell is reduced to V = Vj - rsl', and in the first quadrant we have: j) (qV + rsl'] )- ] I, = Iph - Is [exp kT - I ] = Iph - Is [ exp ( q[v kT I .
h\O, (a)
(b) ! " p
-
r,
t
- I
ts[exp(~H
If = I
ph-i L
Figure XI-17. Electrical circuit of (a) ideal irradiated pn-junction connected with a load resistance RL; and (b) equivalent circuit.
XI Organic photovoltaic devices
335
L
Figure XI-IS. Equivalent circuit for real irradiated pn-junction with (a) series (rs) resistance; and (b) with series (rs) and shunt (rp) resistances.
Furthermore, when leakage currents (which include shunt currents through short-circuits) arise across the cell, we can take into account this component by introducing a parallel resistance (rp) such that rp --+ 00 when leakage current ip ~ 0. We then have: I' = Iph - i - i p = Iph - Is [ex p
(:i)-I] - ~:
Repla cing Vj by Vj = V + rsI' we have: ( q v + rsI' )- ] V +rsI' I - -I, = Iph - Is [exp kT rp
(3)
While for the ideal cell in the external circuit we do not find the total photocurrent (Iph) but only I' = Iph - i, in a real cell the same reduction is more pronoun ced. This is because the shunt resistor Ip introduces the linkage curre nt ip leading to I' = Iph - i - ip. Simultaneously, series resistor consumes the voltage rsI' . In ideal cells, we have r, = and rp --+ 00 : so, the departures from these values give an evaluation of the imperfections of the diode; considering that rs always presents a small value and that r, « f p, we can then estimate the values r, and f p: by differenti ation of expression deduced from (3):
°
( qv+rsI' ) f( I, , V) = Iph-IS [exp kT - ] 1 - V+r rsI' · - I, = 0, p we have:
~ir =
-f, that leads to (with v
dV ] [ dI' 1'-0 -
~
-rs
_
UT
= kT / q ~ 0.024 V):
rp Isrp V 1+ exp UT
(because when I' = 0, V = Voc dV ] [ dI' v=o
(as rs is small)
~ - rs -
»
UT )
~
Isrp rsI' I +-exp UT kT
UT
~
- rs
336
Optoelectronics of molecules and polymers
ideal chara1e~ stic
al characteristic
f
I
/
;.- /--------. / ~
I
- 1 (.d
/
fs
;1
-- - - -::A..
I
ea case:
- I ~-d-~O'\ f s ~ oo an f s
=
v
---
-'--'~:'-:==--------------A~_ _~ Icc
-I (.d al -1 d '\ rp ; I e case : rp =0 an rp~oo
Figure XI-19. Reverse values of series resistance(r;: I) and shuntresistance (rp1) linkedwith the characteristics slope at V = V oe and at V = 0, respectively.
With I = -I', we also have r; 1 = [1~ ]1=0 and rp = [1nv=0' The slopes of the characteristic I(V) under irradiation, calculated for I = 0 (at open circuit) and in V = 0 (at short circuit) give the inverse values of the series resistance rs and of the shunt resistance rp, respectively (see Figure XI-19 ). If r, incre ases, the slope of the characteristic decreases in the first quadrant and Icc also decreases. If rp decreases, the slope increases in the fourth quadrant, and V oe then decreases. l
Note: To take into account a more general behaviour of the current inside the real jun ction (recombination current in the space charge area ), eqn ( I) must be written
) -I]
I
in the form : J = js [e xp (~~4 -Jph, where n is the "ideality factor " (n = in the ideal case). The relationship between Voc and Iph expre ssed in eqn (2) obtained when rs = 0 and rp ---+ 00 , is thus changed to Voc = also modified and becomes
I (I
+ r~) - ~ r p
p
= Is [exp
(~(V nkT
n~T Log
rsl)) -
Cr;+I).Eqn (3) is
I] - Iph .
4 Possible limits
It can be thought that a power conversion efficiency as high as 10% can be reached with organic solar cell s ([Nun 02] and [Peu 03]). Given that
l]
=
FF x l ee x Voe ~e
e
Jcc
= FF x Voc x Ee
= FF x Voc x - x EQE , hv
XI Organic photovoltaic devices
337
then (ef § IV, 2-e): eVoe II = FF x - - x llA x IQE hv
= FF
eVoe x -hv
X
llA x lldiff
X
nrc x lltr x nee-
As nrc . lltr and nee are all close to I (see §IV,I), we can consider the power conversion efficiency (ll) as being essentially the product of 4 terms as in II = FF X (qVoejhv) x llA x lldiff. With small series and shunt resistances (r, < 50 Q andr, > 25 kQ), and FF ~ I (see §IV, 3), we have for the power conversion efficiency. II = e~~c X llA x lldiff. With e~~ ~ o;/e~v = 0.25, llA = 0.5 and Ildiff ~ I, a value we can hope to achieve with appropriate systems [Nun 02], we finally have II ~ 10%. So, with at least 3% power conversion efficiency already demonstrated, and with improvements to reach 10% in the years to come , "plastic solar cells" may significantly contribute to future energy needs .
5 Examples; routes under study and the role of various parameters a Recent results As recent results we should mention Brabec's cell based on PPV and fullerene derivatives : at Siemens , he claims an efficiency around 5% [Bra 04] . Conversely to this wet route , dry deposition with small molecules can also be realised; so, with the structure ITO jPEDOTjCuPc - C60 jCa+AI, we obtained as photovoltaic parameters (Figure XI-20) : Vco = 0.45 V, Jcc = 0.768 rnA cm- 2 , II ~ 1.8% with ITOIPEDOTI3"(15nm CuPc+25nm C60)lAJ
, . . . . - - - - - - - - - -O.OOt-r-- - - - - - - - - - - - - - - ,
..E
1 - - - - - - - - - - -O,OOOS+------ - - - - - - - - "',·- ---1
u
-c g.lJ,6
I c ~
f - - - - - - -- - -
08
0
-0.4
-O,OOOS
1
-"'::--------- - - - - -1
17
:::>
U
'-------------o,.OO t 5~-----------------J
Bias Voltage
Figure XI-20. I(V) characteristic ofITO/PEDOT /CuPc - C60/Ca+AI.
338
Optoelectronics of molecules and polymers
4 mW cm- 2 as luminous flux. As we can see on the I(V) characteristic, an important serie s resistance drastically disturb the measurements; an electron transport layer at the cathode interface could improve the result s. With pure CuPc as an acceptor layer and a BCP layer acting as a blocking layer in relation to exciton diffusion at the cathode interface, J.M . Nunzi [Tro 03] obtained very encouraging results with an interpenetrating network made ofITO/ PEDOT:PSS/ CUPC:C60 (1:1) (40nm)/BCP (8nm)/Al (60nm) with annealing of CUPC:C60 at ISO °C under argon atmosphere for 20 min. Under irradiation of 100 mW cm - 2 , the optoelectronic parameters are as following : Voc = 0.50 V, Jsc = 11.5 rnA cm- 2 , FF = 0.37 and 11 = 2.14 %.
b Improving the photovoltaic properties of materials It could go via the implication of several different technological route s. Here we can cite five examples:
•
•
•
Adapting the band gap ofmaterials to solar light this step is possible using the various , available , synthetic routes to n-conjugated polymers with differing band gap s [Ronc 98]; Orientation of chromophores to generate an internal field An alternative method to effect photodissociation throughout the whole volume of a film was proposed by C. Sentein et al. [Sen 97] . The proposed route implicates the creation of an internal field due to the orientation of chromophore molecules by the continuous application of an external field, in a technique otherwise known as 'poling' . This provoke s in the photovoltaic device an effect of rectification which would stimulate photodissociation. This effect has been shown to improve a mono-layer device, based on non-optimised polythiophene used initially for photovoltaic conversion, by a factor of 40 [Sic 00]; Improving depo sition techniques to increase absorption capacities {Fie 00 J The octamer octathiophene (a -8T) , shown in Figure XI-21, was examined by C. Videlot and D. Fichou . They found that its properties varied greatly with respect to its orientation once deposited on a substrate. A pn-junction, in which the a8-T acted as the p-type semiconductor and a derivative of perylene was used as the n-type semiconductor, was used in the system LTO/a-8T/perylene derivative /Al . Between 400 and 600 nm, a photo-current (Ipe) was generated when the system was illuminated from the ITO side with polarised light. It was found that the current increased by a factor of ten when the a8-T molecules went from being perpendicularly aligned to being aligned in parallel with the substrate. Thi s effect was attributed not only to an improvement in the transport properties of the a8-T,
Figure XI·21. Representation of Cl-8T.
XI Organic photovoltaic devices
•
•
339
but also to a better coupling between the molecules and the incident light, an effect which improved their optical absorption ; Improving charge transport Following the disassociation of photogenerated charges, the problem of their transport to the electrodes, as we have seen, needs to be tackled. Given the low mobility of charges in organic solids, possible solutions may exist in the .use of ordered phases based, for example, on liquid crystals . Furthering this idea, the mobility of electrons being again low in polymers, an eventual solution may rest in the use of mixed organic/inorganic systems , in which the transport of the electron may be assured through the inorganic phase . Doping effect of n or p layers is also studied, as well with molecular materials (dyes) as with the ion beam implantation technique we have previously developed [Mol 98] to realize organic devices (diodes or transistors); Optimising the morphology of interpenetrating systems The optimisation of photogenerated charge separation requires, on the scale of exciton diffusion lengths, a perfect homogeneity of the donor-acceptor system . A solvent free method, using the co-evaporation of p-type oligomers and n-type molecules could reasonably result is such a structure ; the vacuum quality is a critical parameter really. It has also been remarked that the use of composites which exhibit concentration gradients , with donors and acceptors on opposite sides of a structure , should improve the collection of positive and negative charges at the respective electrodes.
6 Conclusion At the present moment there is a considerable push in research into the field of organic photovoltaics and it is with some excitation that more results are expected in the near future . On bringing together the various possible techniques, which are not necessarily exclusive to one another, the short term aim is realise structures which display efficiencies of the order of 5%-6% and have lifetimes of around 5000 hours . Activities based on organic photovoltaics should be possible on an industrial scale. And given the recently published results, researchers could well be there in the next few years.
XII The origin of non-linear optical properties of n-conjugated materials and electro-optical modulators
I Introduction: basic equations for electro-optical effects 1 Context Whilst this book is mostly concerned with coupling electron transport propertie s with emis sion and optical absorption propertie s, this Chapter deals specifically with the effect of an electric field (E), whether static or variable, on the optica l properties of an organic material. In particular we will look at the effect of electrica l fields on the indices of materials, and the changes in the intensity or phase of an optica l wave propagated through a polarised organic medium. The assemb ly of polymer based electro-optical modulators is then introduced. First of all though, as a general overview, we shall detai l the generally observed laws.
2 Basic equations used in non-linear optics [Sal 91] a Standard equations In general terms, a materia l subject to a static or low frequency electric field undergoes certain deformat ions. These typically result from either ionic movements in mineral b ased composites or from electron displacements in organic media (following electronic and molecular orbital deformations). Under the effect of an external electric field, as shown in Figure XII- I, the change in polarisation induces a modification of the optical indice of the materia l at a given frequency. There are two main types of effect that can be observed: • •
when the indice varies proportionally to the strength of the applied field the electro-optical effect is called the Pockels effect; or when the indice varies with the square of the applied field then the effect is called the Kerr electro-optical effect.
342
Optoelectronics of molecules and polymers
-B:fI e----
O~_fiC_ld
Electric field Figure XII-I. Coupling an electric field with an optical field traversing an electro-optical material.
On following the hypothesis that the variation in the indice is small with respect to the applied field, we can use a Taylor type development around values of the indice for when E = O. Using the notation thus: neE = 0) = nCO) = n,
a]
dn) = dE E=O '
gives :
I 2 neE) = n + a] E + -a2E + ... 2
(I)
For the reasons of notation which will become apparent in Section b: r = _ 2a] n3 a2 s = - -3 n
I
are the electro-optical coefficients which are such that: 1 3 1 3 2 neE) = n - -rn E - -sn E + ...
2
2
(2)
Typically, the 2nd and 3rd order terms are small, by several orders, with respect to n.
b The form of electrical impermeability The term electrical impermeability is particularly useful when describing anisotropic media (for example, following ellipsoidal indices). It is defined by 11 = llE r = I/n 2 . As on one side 11 = ~, that is ~~ = ~;, and on the other there is
1 2
~n=n(E)-n=--m
3
1 2
3 2
E--sn E,
we can write ~11 = ( d11 dn ) ~n =
(2 Isn32 ) = rE + sE2. E- 2 E + ... - n3 ) (-21m 3
XII The origin of non-linear optical properties
With
~11
= l1(E) -
11, l1(E)
= 11 + rE + sE 2 + ...
343
(3)
(The coefficients rand s are defined beforehand to arrive at this simple relationship for ~ 11, which introduces the simple coefficients r or s in front of E or E 2).
c Pockels effect and order of size In many materials the term relating to the 2nd order Kerr effect is small with respect to that of the I st order Pockcls effect. In effect:
I 3 neE) ~ n - 2"rn E.
(4)
Typically, r ~ 10- 12 to 10- 10 m y -I , that is from I to 100 pm y-I . If E 106 Y m- I, then the term 1rn3E is of the order of 10- 6 to 10- 4, a very small variation in the indice with respect to the effect E (the usual minerals considered are KH2P04, LiNb03, LiTa03 and CdTe) .
=
II The principle of phase modulators and organic materials 1 Phase modulator Phase modulation means that information, based on either yet) or E(t) , can be transferred using an optical signal by modifying the phase of this optical wave. An alternative method is with an amplitude modulator which varies the intensity of the optical wave by using parallel monochromatic luminous beams, i.e. a laser beam. When an optical beam traverses a Pockels cell of a certain length (L) subject to an electric field (E), as detailed in Figure XII-2, the wave undergoes a shift in phase: 2n
Ao
n(E)L,
(5)
where AO is the wavelength of the light in a vacuum . The introduction of eqn (5) into eqn (4) yields:
Optical field
2n = -nL Ao
2n I 3 -L-rn E Ao 2
=
rn 3EL n--, Ao
(6)
-; d (a)
Figure XII-2. Pockels cell under : (a) transversal (E (E = V I L ).
= V Id ); or (b) longitudinal polarisation
344
Optoelectronics of moleculesand polymers
with
rrrn3 VrrL
(7)
Accordingly, we can deduce eqn (8): }..o d V rr = rn3 L'
(8)
For a longitudinal Pockels cell, as in Figure XII-2-b, the field is now of the form E = V /L and the half-wave voltage, which is commonly denoted by Vkrr' becomes Vkrr = ~~. We can now use eqn (6) again in the form
V V . . - (longitudinal cell) .
(6')
Thus the shift in phase changes linearly with the applied tension. This we can use to modulate the wave traversing the cell. Generally, the value of V~, rt can be of the order of I to several kV for longitudinal modulators. Transversal modulators permit a lowering of the value of V rr through variation of the ratio ~ (d can be several microns and L can be around I em), so that v; ~ I to 100Y.
Comment If the applied field (E = E(t)) varies greatly during the transit time (T) of the optical wave, then obviously the optical wave will be subject to a varying value ofE during its passage through the modulator. The field E(t) which can be used is the
o:+----~---
V
Figure XII-3. Variation in dephasing(
XII The origin of non-linear optical properties
345
Figure XII-4. Positioning of electrodes with respect to the transmission in a transverse modulator. average field Eduring the two instant t and t + T. The size of the modulation band is generally taken as being equal to l iT. In order to limit this problem, the tension (V) can be applied at the side of the entrance of the optical guide so as act directly on the transmission axis . This is schematised in Figure XII-4. Modulation up to several GHz is possible using this technique.
2 The advantages of organic materials Other than the advantage that organic materials have in being easily shaped, they do present other advantages specific to this field :
a Advantages over inorganic materials As the inorganic materials used are normally ionic in nature, the displacement of these charges is slower relative to the movement of electrons alone, especially electrons delocalised in organic media. Ionic polarisation is relatively slow especially when compared to the response times of organic materials, and in particular rr-conjugated polymers, which can be extremely fast (of the order of femtoseconds) .
b Advantages due to the low dielectric permittivity of organic materials (er R:j 2) Figure XII-5 schematises the circuit used to control a Pockels type cell. The generator provides an excitation at low frequencies which is applied to the cell and acts, no less, as a condenser. Its losses are shown in the scheme by the parallel conductance G p . The RC , is small if C is small. This is favoured in organic materials as response time, t their permittivity (E r ) is also relatively small (s, ~ 2) . In addition, we have:
=
Vs Ve fc
I
=-------~
1 + Z(G p + jwC)
I
.
1+ JWZC
.
(With
Gp
«
wC).
The modulator acts as a low frequency filter, with a cut-off frequency (fc ) at (denoting S = [I x L] as the available surface of
= 21t~C" As C = £o~rS = £o£J1L
346
Optoelectronics of molecules and polymers
Figure XII-5. Schematisation of a Pockels cell control unit.
capacitance, see also Figure XII-2), we can see straight away that with organic materials that have a low value of Er , C is also small given that the cut-off frequency is high. Comment On introducing VIt, which insures the phase shift by rt and is such that d ' . !£!::!l. _ n3r _ " . V It -- l!l.. 3 -L' we amve at. v - -Zl 2 - constant, lor a given system. nr
n
It
~~
For any given system in which fc increase, VIt also increases (along with consummation). And the ratio fcAO/V It defines the figure of merit of the modulator.
c The state of the art Y. Shi at the TACAN Corporation, along with his colleagues at the Universities of Southern California (Department of Chemistry and the Centre of Photonic Technologies) and Washington, has shown that by controlling the form of the organic chromophores it is possible to obtain electro-optical modulators having half-wave tensions lower than 1V (V It ~ 0.8 V with VltL ~ 2.2 V em) [Shi 00]. The results also showed a large increase in gain (inversely proportional to Vi). And the considerable decrease in parasite signals allowed the operation frequency to be increased to 1000Hz, equivalent to a transfer of data of 100 Obits s-I . The decrease in VIt was realised by increasing the concentration of chromophores while simultaneously limiting electrostatic interactions (which reduce the electro-optical effect). This was made possible by inserting chromophore molecules containing bulky groups that contributed to steric effects. Other materials, notably those with octapolar charge distributions, have been used in attaining 'giant' non-linear effects [Med 95].
3 Examples of organic donor-acceptor non-linear optical systems Two principal effects are responsible for electronic displacements in molecules [Mer 95]: •
•
the induction effect which gives rise to a preferential attraction for electrons shared by atoms having a-bonds (in a range of electronegativities range based on the capacity of atoms to attract electrons); and a mesomeric effect which brings into play n-electrons or doublets of unshared electrons situated in p-orbitals. These charges can move from one bond to another and are not localised to the extent of electrons in a-bonds.
XII The originof non-linear optical properties
347
a The induction effect Briefly put, when two atoms are bonded by a a-bond, the more electronegative atom tends to attract the electron s in the bond towards itself giving rise to a dipolar moment. In addition, the polari sation effect can be transmitted along a chain of covalent in an effect which dimini shes with distance (and typicall y disappears beyond the third bond). The inducti ve effect is represented by the symbol + -+ with the arrow directed towards the negative end of the dipole, and in the opposite direction to the sign - ----+ +
: Sil·
b The mesomeric effect The structure of a molecule, in reality, is in between the two limited formulas which are both unable to describe the partition of electrons, given that n-electrons are more mobile than a-electrons.
Example: the isolated double bond
The carbonyl group is normally represented by:
""
..o / ;C= ..
Neverthele ss, 0 is much more electronegative than C, and can attract electron s more powerfull y. The following repre sentat ion is therefore also plausible:
""+ C -0: /
The rt-electrons are delocalised towards 0 and, in effect, this situation can only be written using both of the proposed forms. These two forms are called mesomer s and are both intermediate with respect to reality.
c Competition between induction and mesomeric effects and the example of substitution on benzene rings ct Influence of an electron donor: - NHz. resonating with the benzene ring chemic al representation schematises specific effects:
The
(i) a weak induction effect [N (Se" ) is more electronegative than C]; (ii) a strong mesomeric effect through the conjugation of the N free pair of electron s with the benzene ring; and (iii) the pair of electrons on N(:) tend to delocalise towards the ring.
348 Optoelectronics of molecules and polymers Result The electron cloud is delocalised towards the cycle and, in effect, the -N(:)Hz group acts as a donor.
....
(i)
Minor inductive effect (ii)
+
(iii)
.....
+
+
6·--6~"6 Strong mesomeric effect
~ The influence ofan electron attracting group : N02 In the case of N02 there is no free electron pair ready to delocalise towards the benzene ring. With 0 being more negative than N, 0 tries to saturate itself with electrons moving them from the ring. In effect, NOz is an attracting (or acceptor) group.
Induction effect
Mesomer effect
4 General structure of molecules used in non-linear optics [opt 93] As will become apparent when looking at the materials in more real terms, organic molecules which allow intermolecular charge transfer can give rise to a particularly high hyperpolarisability. These molecules are termed 'push-pull' molecules. They consist of donor and acceptor groups linked by a conjugated system, otherwise termed a 'spacer' (S) or a transmitter, as shown in Figure XII-6.
XII The origin of non-linearoptical properties
349
Dfonjugated systemL A (8)
--T
Figure XII-6. Donor-spacer-acceptor system.
III The molecular optical diode Here we will show that molecular optical diodes can in fact give a rectifying effect. Light polarised in one direction can pass, while light polarised in the opposite direction is 'blocked' . An analogue is, of course, a rectifying pn-junction, which rectifies by exploiting effects due to a passing current and the excitation developed by an electric field. In molecular optics, the created electronic response is FE = ndji ( = ~~) in which n is the density of electrical charges and dil = qdl is the dipole formed on displacing by dl an electric charge from its centre of gravity due to the passage of an optical wave. Comment In linear optics, the polarisation is tied to the optical indice by the relationship F = EO(E~ - I)E, with E~ = n2 for non-absorbing media. In absorbing media, = n*2.
E;
1 The centrosymmetric molecule The centrosymmetric molecule contains electrons which are highly polarisable. A good example is that of delocalised n-electrons, as found in benzene (C6H6). dji = qdl represents the dipole moment.
-q
dl
------+)
+q
Additionally, in one dimension, moving a charge (q) by a distance dl superimposes on the system a dipole moment of dil = qdl, as detailed in Appendix A-9, Section III. Similarly, moving a charge -e by -dl is the same as applying a dipole moment dii = edl , as shown in Figure XII-7. In addition, if we move electrons under an Initial electron position
.
Superpositioning a dipole d~ = ed!
Result: displacement of an electron by - ill=- 0'0
ill =0 '0
-8
0/
x
df=e ai 0';-';0 -8 +8
. .
o~ o
-8
-E
+
Displacement can be due to field (E) Figure XII-7. The equivalence of chargedisplacement, polarisationgenerationand vice-versa .
350
Optoelectronics of molecules and polymers
Figure XII-So Representation of the electronclouds in an unpolarised benzene molecule.
electric field (E), with direction -dl, that implies the application of dji = ed! and thus a e,olarisation P= ndji is generated in the opposite direction, depending on dl. If E = 0, the benzene molecule electron cloud has the form described in Figure XII-S o We can now consider the same benzene molecule under an electric field (E), as in Figure XII-9. _ With respect to the axis of time, successive lobe s due to the function P remain symmetric. There is no 'rectifying' effect observed at this size of optical field (E), whether it_be a weak field in which case P is directly proportional to E as P = EO(E r - I)E , or whether it be a strong field in which case the polari sation stays as a unpaired function (with successive + and - lobes) an9 a non-linear effect is introduced simply by the unpaired harmonics at the level of P.
2 Non-centrosymmetric molecules Now we can look at the same benzene molecule which has, however, been modified by the addition of electron donor (D) and acceptor (A) groups so that it has become non-centrosyrnmetric. This modification results in the displacement of the electron cloud towards the attracting, acceptor group. Any effect exerted by an optical field will be exacerbated by orientating the optical field so that it displaces electrons toward s A. Inversely, its effect would be minimis ed by orientating the field so that it tends to move electrons towards D. Figure XII-IO schematises these two, opposing effects . As detailed in Figure XII-II , Fourier analysis of the resulting polarisation wave shows that it contains, that for non-centrosymmetric molecules, a fundamental, a second harmonic and a c~nti n_uous component. In a one-dimensional medium and when the optical wave is E = EW , the term s for the polari sation wave should thus be written in the form :
wherein Xa is the absolute dielectric susceptibility and such that Xa = EO Xr. Here Xr = (Er - 1) is the relat ive susceptibility, hereon denoted simply by X.
XII The origin of non-linear optical properties
351
E strong field
~l-f'--
-- -
....
---""I.--
---7I',--
-- - --.
t
:" -- ---j : I I
first alternation
I
/
I
I
Weak field
I
second alternation
- I
~1
ill --+tdi df 1_
--+
p=
--+ ndf
polarisationunder strong field
e \£) -- -- -
_- - -
polarisationunder weak field
t
.
Figure XII-9. Polarisation by strong and weak fields of a centrosyrnmetric molecule .
3 Conclusion The second order non-linear polarisation (p(2)) is proportional to the square of E (the term E 2 introduces cos 2 cot = 1+C~S2wt) . It is only with a non-centrosymmetric molecule that that either X2 or Xa2 can be zero . In addition to the phenomenological evidence described above, we can also perform a direct demonstration of this effect [yar 89]. _ _ If a molecule is symmetric, then changing from E to -E is effectively the same as moving charges in an exactly similar but symmetrically direction, so:
(I)
352
Optoelectronics of molecules and polymers
fiR E
polarised wave
r '-~ PN !r I~
I
first alternation
exaggerated electron disolacement
!
I
second alternation
I
small electron movement
Figure XII-tO. Polarisation of a non-centrosymmetric molecule .
I
ij Fundamental
Second harmonic
Continuous component
Figure XII-H. Resolution of polarisation wave for a non-centrosymmetric molecule.
XII The origin of non-linear optical properties
353
Additionally, the definition of p(2) gives: }:::} p(2)(E) = p (2) (_ E) p(2)(E) = Xa2E.E P(2)(-E) = Xa2(-E)-(-E)
(2)
And finally: from eqn (1) : Xa2E.E = -Xa2(-E)-(-E)} . ~ E ~ (E~) (E~) :::} Xa2 = -Xa2, that IS Xa2=O. . and from eqn (2): Xa2 E . - Xa2 -
IV Phenomenological study of the Pockels effect in donor-spacer-acceptor systems Here we shall describe a molecular system containing n-electrons and establish , directly, the relationship between modifications of the function indice with respect to the applied field, otherwi se known as the Pockels effect. The establishment of the same type of equation, using more conventional methods , is detailed in Appendix A-II . We will use an optical wave (E W ) which propagates in the Oz direction and is polarised in the Ox direction . Figure XII-12 indicates how the electrodes are placed about the active medium .
1 Basic configuration a Molecular system with prior orientation of It-orbitals in the direction Ox A static polarisation field (Es) is applied using 'poling' , that is to say the field is applied during a descent in temperature of an electro-optical material from its glass transition temperature (Tg) to ambient temperature (T) to give the result shown in Figure XII-l3-a.
b For systems also containing a D-A pair Here we are considering the system surrounded by the dashed line in Figure XII-l3. The electronic cloud is deformed and the centre of gravity for the charges is moved
·z
Figure XII-12. Configuration of an active medium placed between electrodes parallel to the plane yOz and traversed by an optical field polari sed with respect to the Ox direction.
354
Optoelectronics of molecules and polymers
r - - - - - - - - -- - - - -
(a)
I
I D
I I I
I I
I
I --=--:-:r;---
Y
Y Es
I +
A Symmetri cal molecular system. (Centres of atom ic and charge gravitie coincide ).
L
x
x (h) and (c)
(d)
I I
I I
I I
J
D-A system
Figure XII-B. The position of the centre of gravity of electronic charges (GE) for: (a) a symmetrical molecule; (b) a non-centrosyrnmetrical molecule whetheror not (c) in thepresence of an opticalfielddirectedtowards Ox; and (d) the same as (c) exceptingthat the fieldis directed towards - Ox. by x > 0 so that OG E = x. The greater the donor-acceptor character of the additional groups, and in effect the greater the size of the electron cloud, the higher the value reached by x (Figure XII-13-b).
c In the presence of an opticalfield The ions which are attached to atom s within the solid materi al and in effect it is only the electronic cloud which moves, in a manner similar to that shown in Figure XII-13-b , once the sys tem is under the influence of an optical field. The movement of the electron cloud is with respect to its centre of grav ity, already moved by the O-A pair. With GE displaced under the effect of both the O-A pair and the optical field by a distance x we thu s have fr = -kx (Figure XII-I3-c, identical to Figure XII-I3-b).
d The effect of a static electric field (Es) applied in the direction - Ox Here we consider the situation pre sented in Figure XII-I 3-d. The electric field goes against the return force fr and has a tendency to displace GE towards x > O. Thi s displacement occurs as strongly as the charged electron cloud is large due to coupling strength. In effect, as we have seen in Sub- sect ion b ju st above , the value of x tend s to be high. We can therefore write that the force generated by E, is in the form fES = +Ox ; the force fES increases prop ortionally with Es .
e Result of combined forces The result of the force s (fR) with respect to Ox of force s fr and fES is thus in the form fR = fr + fES = -kx + Ox.
XII The origin of non-linear optical properties
355
With k = mW5 and D = m&2 (which is such that &2 ex: Es , as D ex: Es): (1)
fR = -m(w6 - &2)x .
Comment J If the resulting displacement x is, in effect, as large as Es and thus also D(D ex: x), the term Dx = &2x varies similarly to x 2, that is as an inharmonic term. Comment 2 With an optical wave polarised in the direction Oy, the fundamental relationship for the dynamics of the system can also be written for the direction Oy. Here the field E, is put into terms of Oy and this effect may be greater than that in the direction Ox given the anisotropy of molecular orbitals (see Comment 2 at the end of this Chapter, Section IV-4).
2 Fundamental equation for a dynamic system Here we will assume that in the permanent regime under study frictional forces (f t = -mr*.) are negligible due to r « [co - wol (the further from the resonance point we go (co - wo) the more r tends to zero). Therefore, the fundamental dynamic relationship for an electron with respect to Ox is:
(2) W
Only the qE component contributes to the Coulombic force . The effect due to the static field (E s ) was taken into account within the term m&2x, which is included as part of the return force (fr ) as the electronic effect of E, was considered as a modification, or rather perturbation, of the return force . With E W = Eo cos cot, the solution under a forced regime x = Xo cos wt( = xoeiwt that is = -w2x) gives us:
x
w
2 2 2 eE ([wo-& ]-w ) x = - m
3 Expressions for polarisability and susceptibility With N as the electron density, a polarisation of P caused by the displacement of electrons by a distance x along Ox can be determined using P = -Ne x Ux and 2 w2 = Ne in p
com
(3) Typically, we set
w2 X.w =
2
P 2'
wo-w
(4)
This is the term which appears in a linear polarisation of a system not subj ect to an additional static polarisation (E s ) ' In this case , we have fES = 0 and the term in 1)2
356
Optoelectronics of molecules and polymers
disappears . The eventual expressions of the polarisation (p(w)) is thus in the form: -(w)
p
2
wp -w -w = £0 wo-w 2 2 E = £OXw E .
On assuming that 8 is small with respect to [co - wol, placing it outside of the resonance zones. And on using eqn (3) then with eqn (4): (5)
4 Expression for the indice-and the insertion of the electro-optical coefficient r With £r = n~ = I presence of Es :
+ X, we have as a relationship for
On introducing nw = .)1
the indice in Ox and in the
+ Xw, the indice in Ox and without E, gives (6)
Finally: (7) 2
· h Xw = ~ h WIt 2 ' or rat er 2 wo-w
As nw = .)1
1
-2-wO- w2
2 2
Xw, we h ave un A xwS- . = = nx - n., = -
+ Xw {} Xw = n~ -
w~
2nww~
1, we can write
(8) As indicated above, 82 ex: Es = aEs, so that to a first approximation-neglecting I in front of n~ (given that with the presence of chromophores the medium is, intrinsically,
XII The originof non-linear optical properties
357
highly polar so that its permittivity (s, = n~ ) can be relatively high by even 3 or 4 orders)-we have: n4
~n ~ ~a 2nw wp
~n in which r
== rp ~
Es ,
in which ~n is in the form
I
= 2 m3Es
~ Wp
(9)
and is the electro-optical coefficient, and n.,
== n by notation,
an indice following the direction of the polarisation of the optical wave and measured in the absence of the polari sing field Es . ~n is proport ional to Es , and eqn (9) is identical to eqn (4) and well characterises the Pockels effect. Comm ent 1
as d
There is another, possible way to represent the Pockel s effect:
(:2) = d(x - 2)= -2x- 3dx, we can write
~ (:2) =Id (n12)1=2n- 3~n =2 ~~
and on using eqn (9) leaves
~ (:2) = rEs ·
(10)
Here we recover the classical expression used to define the electro-optical effect, which was evolved from the ellipsoidal deformation of indices at a low frequency electric field (linear variation within the electric field of coefficients
[n'r 1from an
ellipsoid of indices). Comm ent 2 Variations in the indice due to the application of E, can themselves be variable. This depends on the orientation of the static field E, with respect to the direction of polarisation of the incident optical wave and anisotropic effects can appear. However, in reality it can be advantageous to polarise the wave in the direction Oy perpend icular to E, (which follows Ox). The deformation of orbitals by Es , only for the propagation of the same wave but polari sed in the direction Ox, can have a greater effect on propagation along Oz than along Oy. In the adjacent scheme, we can see that the p-orbital retains the same elongated form in Ox (admittedly slightly longer in the presence of Es ) , but is also much 'skinnier' in the presence of Es .
~ lx
.,0
358
Optoelectronics of molecules and polymers
V Organic electro-optical modulators and their basic design 1 The principal types of electro-optical modulators An electro-optical material can be used as a polarised wave phase or amplitude modulator depending on the design geometry chosen.
a Phase modulator The phase modulator demands the more simple structure . It consists of a modulator arm constructed from a simple optical guide, onto which the incident wave falls. The modulation is performed by applying a transversal tension, which induces a phase delay (~
b Amplitude modulator Phase shifting alone does not change the intensity of the optical wave subject to modification. However, here, the modification of the intensity of an optical wave is possible by using, for example, a Mach-Zehnder amplitude modulator. This device can be inserted into an arm of an interferometer. As shown in Figure XII-IS, the amplitude of the incident wave (L) is equally shared into two waves, each with intensity! Ii, down two arms neither of which have been subject to an electrical field E. The from of the modification induced by E on
Exiting li&ll' mod ulated by E
Figure XII-14. Schematisation of a phase modulator.
XII The origin of non-linear optical properties 359
7
electrodes =>cos 6'1'
Figure XII· IS. Schematisation of a Mach-Zehnder type amplitudemodulator.
1
one of the arms is Ii cos Ll
1 1
J"
2 cos 2 x ~"21 ( 1 + 1 - 4X ) = I - x 2,
2
Ll
and
x
= 2'
we can obtain: 10 = Ii [1or in other terms, ~
=1-
Ll:
2 ]
= t, [1- 4~; y 2] = Ii -
Kliy2,
Ky2.
If Y = Yo cos cot, then y2 ex: cos 2 wt ex: cos 2wt , and thus ~ ex: C I The intensity 10 is thus modulated by a frequency 2w.
-
Cz cos 2wt.
2 Figures of merit As already described in Section 11-2-c, the half-wave tension, in the form Y Jt = d Ao ~ -L for a transversal polarising modulator, should be as low as possible (in rn principle around 1V). Y Jt is often used to characterise the performance of a modulator. Given the expression for Y rt - in order to decrease this parameter it is in our interest to decrease the coefficient ~ and in effect increase within reason the length of the modulator arms. d is normally around several microns and L ~ 3 em . In addition, the factor m 3 needs to be as large as possible to decrease Y Jt, and can thus also be taken as a figure of merit as in FM = m ', and is expressed in pm y -I . Figure XII-16 shows the figure of merit as a function of the wavelength of the optical field for several different materials (from [Bos 95]). Figure XII-I? shows the general configuration of optimised stilbene and benzene in addition to values of rand n at given wavelengths of light. D and A, respectively,
360
Optoelectronics of molecules and polymers
Figu re of
l1le~
-------
10'
KnhO.1
Optimised st ilhene 101 Optimised benzene
"-----------=--, avele ngt h (nm)
500 Figure XII-I6. Figure of merit MF
= n3r (pm V-I) as a function of 'f. (nm).
D-O--A Optimised benzene r (501 run) n (501 om)
=210 pm yol =2.2
Optimised stilbene r (579 nm) 1150 pm V·I n (579 nm) 2.4
= =
Figure XII-I7. Configuration of optimised benzene and stilbene with example values for r and n.
Acceptor A CH3 CN
OCH 3
Donor D NH z N(CH)3
12
20
56
60
35
67
197
218
Figure XII-IS. Values of ~ (10- 4 m V-I) for D-C6H6-A with varying donors and acceptors
A ('f. = 1064 nm) (from [bos 95)).
XII The originof non-linear optical properties
361
donor and acceptor group s exhibit efficiencie s in the following orders: D, N(CHh >
NHz > OCH 3 > OH ; and A, NO > NOz > CHO > CN. The second order molecular polari sabilitie s (B), expressed in 10- 4 m V-I , are given in Figure XII-18 for various para-substituted benzenes. ~, which is also called first order hyperpolarisability, is defined by the relati onship:
p = 110 + Eo([a jEf + [ ~ j Ef Ef
+ [vjEfEf Ef + ...)
in which 110 is the dipole moment of the fundamental state, without deformations and therefore without contributions from the various first [a], second [~j , third [vj and so on orders of polaris abilitie s. raj, [~j and [vj are tensors in effect and Ef is the field localised at each molecule. Macro scopic polari sation follow s the form (see also Section IlI-2 ):
Once molecules are organised in systems with centre s of inversion, resulting in centro symmetric dispositions, strong, microscopic non-linear effects (high value of ~) become ineffective at the macroscopic level (XaZ is small).
3 The various organic systems available for use in electro-optical modulators a Benefits and losses with organic media As already mentioned in Section II, polymers exhibit several attractive qualities with respect to their use in electro-optical devices such as their low cost, their ease of synthesis and manipulation (using spin-coating techniqu es for example) in addition to their interesting physical characteristics, which include their low functioning voltage and dielectri c permitti vity (Er or the order of 2 to 4), the latter of which makes it possible to envisage a good adaptation to the respon se times between the electrical excitation and the optical wave. Certain inconveniences found with these materials should, however, not be ignored . They include the elimin ation of the isotropic character in organic (amorphous) media, most notably in polymers (rt-conjugated included) which tend to form centro-symmetrical systems in which non-linear second order effects also tend toward s zero. In addition, in order to activate the non-l inear properties, ' poling' microscopic aggregates with an electric field is necessary. Any alignment of such aggreg ates breaks down the centro- symm etry. The material does, however, retain a certain instabil ity due to the ability of thermal effects to agitate and disorientate any aligned aggregates. The stabilisation of ce ntro-sy mmetry is the main cause of problems at an industrial level, especially when the material s otherwise exhibit high chemi cal resistance, and a reasonably low sensitivity to humidity and to oxidation of n- bonds. For the present moment , one of these materials used in organic modulators is polyimide [Gar 99j.
362
Optoelectronics of molecules and polymers
b Thedifferent systems Most crystallineorganicmaterialsare centro-symmetric and thus uselesswithrespect to second order effects. Non-linear moieties are thus often used incorporated into an amorphous polymer, which is vitrified directly following preparation into a film. The electro-optical performances are conditioned by the concentration of the chromophores (non-linear D - n - A moieties) used which can be inserted into the final material. Different systems, using this technique, can be prepared: •
• •
'guest-host' systems, as shown in Figure XII-19-a, are prepared from a mixture of an optically active medium mixed with a polymer (which necessitates solvents such as toluene or chloroform). Solubility parameters control the final chromophore concentration; systems prepared by grafting chromophores onto the back bone of a polymer, as detailed in Figure XII-19-b; and covalent systems obtained via the formation of covalent bonds between chromophores and polymerschains, as shown in Figure XII-19-c.
A stepcommonto the use of thesesystems is that once preparedthechromophores must be alignedso that the material loosesas muchas possibleits amorphous character and improves its electro-optical efficiency. The effect of this procedure is shown in Figure XII-20-a and -b for guest-host and polymer grafted systems. In order to
(a)
(b)
Figure XII-19. Different possible systems: (a) 'guest- host'; (b)chromophore grafted to back bone chain; and (c)chromophore inserted into polymer chain.
XII The origin of non-linearopticalproperties 0
363
0
;01
,
;01
>
w (a)
0 ;01
,
»
w
(b)
Figure XII·20. (a) 'Ouest-host' and (b) grafted systems, after chromophore orientation by 'poling' .
get around this stage, or to stabili se the orientation obtained by using this method, mesogens (polymer mesogens) can be used which orientate themselves in a given direction (in the liquid crystal state) . In theory though it seems that this latter method may not give satisfying electro-optical performances.
VI Techniques such as etching and polyimide polymer structural characteristics 1 Paired materials: polyimidelDRl As a material for a polymer matrix, polyimide presents numerous advantages including its low optical losses, low water permeability, low refraction indice (1.56 at 1.3 urn) and dielectric constant ( ~3 .2 to 3.5) and good thermal stability (T g = 290 "C). The method used for obtaining films has been well establi shed . In the case of polyimide 6FDA /ODA (otherw ise known as PI 2566 and supplied by DuPont) which is detailed in Figure XII-21 , an adherence promoter is used first of all (VM 651 promoter spread at 2500 rpm for 30 s), then an initial layer of PI 2566 is spread at 500 rpm for 5 s, and then finally the PI 2566 is spread at 200 rpm for 30 s. Following this step is an annealing step at 120 °C for 30 min on a heating plate and then a second heating stage at 300 °C in an oven for at least 1 h. Turning to one-dimens ional chromophores, a good example and representative molecule is Disperse Red One (generally called DR I) (Figure XII-22) , a well known
Figure XII-21. The monomer unit structure of polyimidc6FDA-ODA (PI 2566, DuPont).
364 Optoelectronics of molecules and polymers DRl:
Figure XII-22. The structure of DR!.
nitroa zobenzene based dye. It has been well characterised arid widely used for the last decade.
2 Devicedimensions-resorting to lithography a The dimensions a Intensity modulator Figure XII-23 shows the commonly used Mach-Zehnder configuration for an amplitude modulator. The sizes, shown in the Figure, have been determined with respect to both guiding conditions (mono-mode) and the need to produce a significant electro-optical effect. Assuring the length of the component (to obtain the required effect and reduce VIt), while retaining a guide depth of around 1 micron (to verify guiding conditions) complicates the experimental preparation of such a device . Lithographic masks are used which have to work well at very different scales: of the order of microelectronics and of the order of several centimetres. The technology used for motifs results in poor quality preparations. ~ Phase modulator The simplest device to prepare is that based on a single arm, as it consists of an optical guide sandwiched between two electrodes. In order to obtain a good electro-optical signal and to have appropriate guiding conditions, the dimensions of the device can resemble those shown above for the amplitude modulator. A simplified component can be obtained by using a cladding material to cover over the device made from a polymer which rests in contact with air. This type of guide can be particularly useful in determining losses due to the polymer (such as polyimide, polyimidejDRl etc.). The geometrical form of the guiding conditions were determined by Petermann [Pet 91 and Pet 96]. With the expression
I .S ~m 1\ - 250 ~m }rE~;;;~------------~---· j,{-- ---Wll\1!" -------- ----~
Figure XII-23. Dimensions of a Mach-Zehnder amplitude modulator.
E it wan
XII The origin of non-linear optical properties
365
the mono-mode guiding condition is tjh
w
R = - < 0.3 + ---;===~ h -
) 1 - (tjh) 2
Definitions of parameters for these equations are detailed in Figure XII-24 . For polyimide using the parameters detailed above, we have H = 1.49 (which holds well to the condition H 2: 1) and R = wj h = 1.25, a value below that derived = 1.44. from 0.3 + I- (t/h) The distribution of field lines, obtained equally well from calcul ations or experiment , is shown in Figure XII-25-a. What is particularly interesting is the way in which the lines are well confined within the rib guide. Figure XII-25-b shows the critical evolution of the ratio w j h with respect to h for different values of the coefficient r = tjh for a ribbon guide. A mono -modal regime is reached when (wj h) = 1 for r = 0.5. For polyimide, when r = 0.75 and (w jh) = 1.25 the mono -modal regime is attained.
k
3 Etching Once the dimen sions of the device s have been determined, they can be prepared by photolithography (see Chapter VIII, Section II-2) using masks of an appropriate size and quality. Given the research already gone into preparing etched surfaces exhibiting vertical walls, in principle it should be possible to use dry etching techniques to attain an excellent level of anisotropy. The speed at which the etching can be done depend s on the rate of pulverisation, which in itself depends on two component parts . One is physical and is based on the inert ions used such as argon, and the other component is chemical and is based on reactive reagents , for example oxygen ions used for polymer etching. Appendix A-9 detail s the principal mechanisms and characteristic parameters used . As described therein , the etching of polymers (polyimides) by ion beam s used for microelectroni cs must be performed using parameters close to those used in plasma etchin g (RIE etching). Figure XII-26 indicat es (for polyimide PI 2566 ) the rate of etching speeds with respectto the energ y (E) of the incident ion beam (3 keV :s E :s 6 keV). With a current density J = 0.4 rnA cm- 2, and a liqu id nitrogen trap set close to the sample so as to .-'" -_ ,, ,, , ,,
.
-_
-. ,,
,
"0=I: ail' " . = 1.56 : Polyimid e
": =1.45: SiD :
Figure XII-24. Parameters used in the Petermann conditions (mono-mode guide).
366
Optoelectronics of molecules and polymers
Iulti-rnodc region (a)
r=O.8
2
L...--_......,,
..:L.. . .
(b)
h
Figure XII-25. (a) Distribution of fi eld lines in a rib shaped guide; and (b) mono- and multimode regions.
cool the sample, limit its degradation, trap excess reagents and condense reaction products, a comparison of etching speeds has been performed for various ion beams (see also with Figure XII-16 in which the characteristics of the techniques used are shown), including: • • • •
dry etching using Ar + ions; Reactive Ion Beam Etching (RIBE) using 0 + ions without a trap; Ion Beam Assisted Etchin g (IBAE) using Ar " ion beam with a flux of molecular oxygen; and IBAE with a beam of 0 + ions and a flux of molecular oxyg en. As we can see in Figure XII-26:
• •
the differen ce between dry etching and RIBE etching is as great as the energ y E is small; and there is a step between the optimised energ y for RIBE etching (E :::::: 3 keY) and the energy used for the optimised IBAE process (E :::::: 6 keV). Thi s differen ce can be accounted for by the energy of 0+ ions which generate reactive species (0 ·) by colliding with the oxygen flux. The energ y transmitted throu gh colli sions
en
-
g>
E
"0 Q)
Q) c. ..... I
.s
:c .« ........ (.)
W
1400 1200 1000 800 600 400 200
a 2
4
6
Figure XII-26. Etching speeds compared using different techniques.
XII The origin of non-linear optical properties
367
between 0+ and 0 is of the order of 3 keY (taking into account the kinetic transfer coefficient y = 1/2), in precise equivalence with the energy of 0+ ions used to optimise 0+ RIBE etching . Finally, the optimised parameters obtained were : RIBE 0 + etching: E = 2.5 keY (with J = 0.4 rnA cm- 2 and realised using a similar method [Mou 00)); and IBAE 0+ etching: E = 6keY (with J = 0.4mAcm- 2 realised also for an ion beam current density) .
• •
4 Examples of polymer based structures [Cor 01] a Polyimide guide (as passive material) and characterisation of optical losses
11,,=
5~m
t um
6~m
I
280~~
I .....-------.. 6FDAIMPDA n, = 1,.575
t
4~m
L+":;"'~
' iO z n1 = 1.46
Si Ori entated
< 100>
" Figure XII-27. Geometrical structure of electron microscopic image of a polyimide guide.
c
.9
e.o
I
.g '"
,. ..et,
, L-
. .P. (a)
...J
"
11'I x-axis on guilt: (arbitrary unit)
,)Oz•
(b)
Figure XII·28. (a) Appearance of transversally diffused light; and (b) the corresponding absorption of the optical signal along the guide length.
368
Optoelectronics of molecules and polymers
P(db) =10 loglO(Po!Px)
· 12 dB {
19 18 17 16 15 14 13 12 11 10
PI 6FDA/MPDA
_.
-
-,
- - - ,...--
.,..,
-. -
,... .
-
-0
0.5
1
1.5
2
2.5 X (em)
Figure XII-29. Measuring propagation losses using the 'cut-back' method (LPropagation :::::: 2dB em-I).
b Modulator structure with polyimidejDRI as the electro-optical material
400nm
6pm
3pm
400nm
280pm
(u )
I •
Figure XII·30. (a) Scaled representation of a polyimidejDRI phase modulator; and (b) light injected into the same phase modulator equipped with electrodes.
VII Conclusion Using electro-optical materials such as lithium niobate (LiNb03) [Pap 85], the method by which modulators worked was well understood from the beginning of the 1980 s. However, the rapid development of active organic materials during the last decade or so indicates that completely organic modulators will be soon available. These hold the promise of being relatively cheap to fabricate and could be used in fibre optic networks either directly with the user or through a Hertzian process. Their exceptionally fast response times, originating from the electronic processes involved, will probably be required in response to the demand placed on communication systems, a demand
XII The origin of non-linearoptical properties
369
LED (a)
R emitter
(d) (b)
Rar e earth
hv radi tive
(c) Transfer from ligand singlet and triplet sta tes to Er (possibly 100 % ?)
Fundurnental level
Figure XII·31. Future prospects: (a) schematisation of an all-organic electro-optical device; (b) schematisationof an emitter; (c) principal of erbium emission; and (d) photolithography of polyimide which may permit network fabrication .
necessitating a doubling in optical telecommunication networks every 18 months in a process nicknamed ' Moore 's optical law' [Tou 01] . Figure XII -13 shows the possible structure of an all organic device [Umop 99]. The emitter could be fabricated using the layering shown in Figure XII-13-b and using the current knowledge detailed in Chapter X. The transfer of singlet and triplet states from the ligand q to erbium could be highly efficient, as detailed in Figure XII -13-c . The filter, within a network, could be fabricated using a focalised ion beam (FIB) machine,
370
Optoelectronics of molecules and polymers
giving 1.5 urn mono-mode guides with polyimide derivatives. Figure XII-13-d shows a photo of the derivative 6FDA-ODA as a pertinent example. The electronic servocontrol needs to be constructed taking into account the behaviour of the polymer based electro-optical modulator. In simple terms, experiments are devised in order to model derivatives and their characteristic behaviours and any secondary opposing reactions. In order to measure the dephasing attained at a given applied and continuous tension, a triangular and periodic signal can be directed at one arm of a Mach-Zehnder device . Then the modulated sinusoidal exit signal is recorded and once again another triangular tension is applied but this time with the continuous component. The recorded signal, again sinusoidal can be compared with the previous signal and the difference in the two accorded to the continuous component. We can finally say that the actual progress made recently will allow the fabrication of such devices without any major obstacles. As we have already mentioned, one problem does remain and that is the stability of organic materials. The continuous improvement in their qualities should, however, allow the emergence of devices very early in the 21st century.
Appendices
A-I Atomic and molecular orbitals
Introduction This appendix proposes a relatively simple construction of atomic and molecular orbitals for a covalently bound solid. And is aimed at readers relatively well versed in phy sical electronics. An example is made of the hybridi sation of carbon orbitals.
I Atomic and molecular orbitals 1 Atomic s- and p-orbitals Speaking approximately and with respect to atomic orbitals, we can imagine that each electron within an atomic move s in a spherically symmetrical symmetry. This is the result of a potential from the nucleus which varie s with I/r, represents the overall effect of all other electrons and is, to a first approximation , spherical. The electronic state is represented by the wave function (\IIn,l,m) which is dependent on the three quantum numbers n, nand m. The energy level depends only on n and I while the degree of degeneration is equal to the number of values taken on by m. When I = 0, the atomic orbitals are called s-orbitals and the wavefunctions vary only with n, as in \IIn,l,m = R(r)8 (t)) (
=
=
When I 1, m -1 , 0, I and the orbitals are called p-orbitals: m = 0: 8 1,0 = (J6/2) cos e and <1>0 = 1/ J21t m = 1: 81 ,1 = (J3/2) sin e and <1>1 = (1 / JJ!) cos
374
Optoelectronics of molecules andpolymers z
z
y
)'
x
x
Figure 1. s-Orbitals. If R(r) represents the function Rn , ] , as m varies, invariably the wavefunctions for the three preceding p-states are of the form: (I) : llIo =
~2'1II-; R(r) cos e
Iff .e '
(III) : Ill_I = -
2
Iff
(II) : Ill] = - -R(r)sinecos
-R(r) sm sm
If we set R(r) = R(rr) so that rr has a value defined by the relationship J~f IR(r)1 2r2dr = 95% (which indicates that the probability of an electron being
within a sphere of radius rr is equal to 95%), then we can say that the three equations represent the orbitals in a conventional manner.
Comment It is worth noting the placing of points M as defined by III = OM in Figure 2. As an example, we'll use the relatively simple relationship I
(3
---+
llIo ="2'1 "2R(r)cose = II OM II = OM. Here D is at the origin of the Oz axis, where cos e = I, and therefore OD = i[irrR(r) . Now OM = ODcose. If e E [0, n /2], OM > O. The M points are now placed with a varying e in a sphere above the plane (xOy). If e E [n /2, rr], cos e < 0, then the M points are in a sphere below (xOy). The signs of the orbitals llIo, Ill] and Ill_I can be obtained directly from the signs taken by the variables x, y, z.Todo this, we can use the relationshipbetween spherical
---7l:iI~-""' )'
p,·Orbital
Figure2. Shape of thepz-orbitaI. The + and - signs concern ljJo which follows cose.
A-I Atomic and molecular orbitals
375
z
m
Figure 3. Axes normally used for spherical co-ordinates.
co-ordinates and the Cartesian co-ordinates indicated in Figur e 3:
x . - = Sin 8 cos
. 8 . - = Sin Sin
z
- = co s 8 r
So for example, if cos 8 < 0, then z < 0 and Wo < O. For f er) =
~ R~r)
1ft
> 0 (with r :::::: rj ), the functions Wo. WI and W_I can thu s
be written in the following way:
= X = x f er) = wpx (Wpx > 0 or < 0 depending if x > 0 or x < 0) W_ I = Y = Y f er) = wpy (Wpy > 0 or < 0 dep ending if y > 0 or y < 0) Wo = Z = z f er) = wpz (Wpz > 0 or < 0 depending if z > 0 or z < 0)
WI
We can at last schematise in Figure -4 the s- and p-orbitals usin g r fixed to the value rr (whic h is such that f~r r 2 IR(r )1 2dr = 95 %): To co nclude, the s-orbitals are non-directional , unlike the p-orbitals.
Comment The orbitals we have shown so far concern only one ele ctron per orbital. They are the orbitals wh ich we will go on to use when con stru ctin g molecular orbitals from the sharing of one electron per atom in co valent bonding. However, if we were z
z
z
).
x
Orbital odal plane
x
ns
x
np, (y 0 z)
x
np),
np,
(x 0 z)
(x 0 y)
Figure 4. The ns and np orbitals. Note: the nodal plane is the plane in which there is zero probability of finding an electron.
376
Optoelectronics of molecules and polymers
to consider atomic orbitals which contained more than one electron, or i electrons, then the orbitals will take on the form \II = TI i\IIi in which \IIi are the wavefunctions for each electron. Prior to being anti-symmetric (Pauli), these \II functions are used in the Slater determinateform. 2 Molecular orbitals
Hi
a The example of the simplest molecular system
In the simplestscenariowe ignorethe possibleoverlapping betweenadjacentorbitals, which would otherwise have to be taken into account using the supplementary condition aE/ak = 0 in which energy is minimised following a variationmethod.With the two nuclei in our system placed-and fixed-at RI and R2 and the sharedelectron at r, as shown in Figure 5, we have the Hamiltonian for the system !i2 e2 H = --b. ~ 2m 41t£0(Jf - RII)
e2
41t£0(lr - R21)
If
Hi
• •
if the
---+
electron is localised on the nucleus (1), then
If the electronis localisedin betweenthe two nuclei, then the solutionhas to come from a mixtureof the two precedingstates. Wecan thereforelook for a wavefunction
Hi
HI
+ C2
= Elc,
+ C2
On multiplying the left of the equation by (
-e D
(2)
r
(1)
Figure 5. Layout of ions and the electron in
Hi.
A-I Atomic and molecularorbitals
377
On using the simplifying assumption of negligible overlapping, i.e. S = (
Similarly, on multiplying the left hand side of the same equation with r (
+ C2
°
(IV); and
(H22 - E) = 0.
(V)
In addition: •
we know that the wavefunctions
•
the problem (and thus also the Hamiltonian) remain invariant by permutation of the nuclei A (indice I) and B (indice 2), so that HII = H22 = - Ct.
As the system of the two eqns (IV) and (V) contain two unknowns, the solution is admittedly non-trivial as its determinant is zero. Using our notations, we obtain the equation (o + E)2 - ~2 = 0, which gives rise to two solutions for the energy (o + E) = ±~ that can be written using the form: EL = -Ct - ~ (the lowest energy corresponding to a bonding level as Ct and ~ are positive); and EA = -Ct + ~ (the highest and therefore least stable energy, corresponding to the anti-bonding level). In passing, we can just note that EA - EL = 2~. On inserting EA into eqns (IV) and (V), we obtain (cj + C 2)~ = 0, that is CI = - C2 = CA . In the same manner, on placing EL into eqns (IV) and (V), we discern (- CI + C2) ~ = 0, that is to say CI = C2 = CL . The wavefunction of the Hi system will allow us two solutions which can be written in the following way: \ilL = cd
\ilL =
.J2 (
\IIA =
.J2 (
I
-
378
Optoelectronics of molecules and polymers
As shown in Figure 6, a schematisation of these wavefunctions is quite possible. It is of interest to see that for the bonding solution, the electrons displays a very high probability of being between the two nuclei so that the strong electrostatic attraction between the electron and nuclei (I) and (2) bonds the entire system. However, we can see in the anti-bonding system that the electron displays a high probability of being on the outside of one of the other nuclei so that the strong electrostatic repulsion between nuclei (1) and (2) is destabilising. Comm ent
With S = <
III _ A -
EL=---
EA=---
<X + ~
I+S
<X -~
l-S
b The molecule H2
In H2 there are two electrons which we can assume are placed at the same potential as the electron in the previous exampleof Hi ' as to a first approximation we can neglect the interaction potential between the two electrons. Each of the two electrons has availableto it two orbitals (IlIL and III A)' The system with the lowest energy would be with both electrons each in a bonding orbital. In this 'l'L. :
•
..
Wavefunctions
/~
I . '" ~ ~ • • ~..
CP.I ,
I"
•••••'
6 ' I '
• _,2
_
/
_.'
2
Probability of presence
....-
---
......- - -
, \,
,
1 "
•
\~
} 'A
__z
~ ,.. ,-- -
.
.
Bonding and anti-bonding orbitals (equi-energy curves)
Figure 6. Wavefunctions and orbitals in Hi: left and right, respectively, bonding and antibonding orbitals.
A-I Atomic and molecular orbitals 379
<;"
EA
<;'.
~@ ~
~~ i----:'--«'----=-..l~ ~d" Independent hJdrOJ:en atoms denoted I and 2
Degenerate enel'J:Y level for as) . lem of 2 independent 01001
;::
Bonding and anti - Prohabllity of presence bonding energy densities for bonding I odenslty surfaces for: (a) antilevels as aloms I and unti-bondlng states and 2 come close bonding orbital; and (b) bonding orbital
Figure 7. Energy and electronic states in H2. state, with the electrons localised around the position between the two nuclei, the system energy would be minimised as the electrons would benefit from an attracting potential (negative potential energy) due to the overlapping of Coulombic potentials developed by the positively charged nuclei . This charge localisation (and the maximum electronic density between two nuclei) is the very basis of the concept of covalent bonding. When looking at the overall system, the combination of two hydrogen atoms resembles the melting of one into the other with the final result of an increased local probable electron density in between the two nuclei . The bonding state is again realised using a linear additive combination of the individual orbita ls of each atom , as shown schematically in Figure 7. The wavefunction can be written, generally speak ing for both bonding and anti-bonding states , as \II = c\ (jJ1 + C2(jJ2 and result s from the linear combination of atomic orbitals (LCAO) .
Comment
-
While the function
\IlL
is symmetric, the function \II A is antisymmetric.
on the EL level, the spins are anti-parallel so as to distinguish the two electrons (undistinguished from the point of view of the orbitals as \IlL remain s unchanged if they are permuted) so S = 0 (singlet states); on the EA level, the spins can be parallel as they are distinguished at the level of the orbital (\II A changes sign if the two electrons are permuted) so S = 0 or I (singlet or triplet states).
decreasing
potential Is
Is
energy
Figure 8. Is (J- and (J* -orbitals.
380
Optoelectronics of molecules and polymers
A
D
Figure 9. 2p (J- and (J* -orbitals.
3 a- and n-bonds a a-bonds Sigma (a) bonds are those which have as axis of symmetry the straight line in between the two covalently bonded atoms. For example, from a pair of s-orbitals we can derive the (o-orbitals shown in Figure 8. If the axis Ox is that on which the two atoms (A and B) are placed, the 2p orbitals will have the combination shown in Figure 9. With 'lJL = ~('lJA2Px + 'lJB2px) and 'lJA = ~('lJA2Px - 'lJB2px) '
A
B ()
AD
~
b
~
o
1t·2p.
1t 2P.
A-I Atomic and molecular orbitals
381
b n-bonds n bond s are molecular orbitals which have a plan of symmetry which passes through the straight line Ox joining the atoms and is perpendicular to the direction Oy for n2pz-orbitals or the 'direction Oz for n2py-orbital s, as shown in Figure 10.
II The covalent bond and its hybridisation 1 Hybridisation of atomic orbitals
a What is hybridisation? Imagine a carbon atom with the atomic configuration IsZ2s z2 pz. While it should behave like a divalent element, as in COz, the same configuration does not explain how CH4 comes to exist in its tetrahedral sp3 state , how CHz = CHz exists in its triangular hybrid sp3 state nor how CzHz presents a diagonal sp! hybridisation. These structures can be interpreted on realising that when two carbon atoms are 'united', the valence states of each carbon atom (2s and 2p) are in effect presented as one s and three p orbitals. This first excited configuration (l sZ2 s 12 p3) is favoured if the energy levels of its constituent orbital s are lowered on its formation, and this is what happen s when they are 'mixed', or rather, hybridi sed. The general form of molecular orbital s derived from the process of hybridisation can be written using quite self-evident notations (here carbon atoms A and B are identified by I and 2, respecti vely): I\II} =AII2s}\ + AzI2px}' +A312p y}( +~ 12pz }' + B 112s}z + Bzl2px}z + B31 2p y}z + B412pz}z = I\III } + l\IIz}·
b Different degrees of hybridisation There are indeed different levels of hybridi sation-different levels of coupling of each of the various and involved orbitals. Diagonal spl hybridisation Px orbitals gives:
This sort of hybridisation, involving for example s- and
I\II} = AI12s}, + Azl2px}1 + BII2s)z + Bzl2px}z = l\IIl } + \\IIz }.
in which I\II d and I\liz} corre spond each to 2 possible orbital s to give a total of 2 bonding cj -orbital s and 2 anti-bonding -orbitals, So I\III} can thus correspond to l\IIll} = aIl2s}I ± azI2px}' or to l\II la} = a; 12s}, ± a;12px}\ and in both cases the + and - give the signs of each of the pairs of hybrid orbital s. The resulting n-orbitals are obtained with respect to both Oy and Oz, as shown in Figure II.
a:
382
Optoelectronic s of molecule s and polymers
7t"2p, 2 anti-bonding n· ·orbitals and 2 bondi ng n-orbi tals
7t 2p, 7t"2p, 7t 2p, Figure 11. rr" and rt-orbitals.
Triangular sp2 hybridisation The system couples only the states 12s > , 12px} and 12py} while leaving the state 12pz} outside of this linear coupling. The coupling can thus be written:
+ A212pxh + A3/2p y} I + Btl 2sh + B212pxh + B312p yh
\II = A112s}I
= I\III}
+ 1\II2}
The three hybrid orbitals have their axes in the same plane and are generally denoted 2spi , 2sp~ and 2sp~ . In a plane perpendicular to these is the fourth orbital, 2pz, which gives rise to the rr-orbit al, For the molecule C2f4 below, the orbit als are schematised in Figure 12.
H ---..C ==C/H
H---
~
The angle s between the three hybrid a-orbitals, which originate from the same carbon atom, must be 120 o . A calculation performed in the same manner as that shown in the following Section 2 (for the sp3 hybridi sation), allows a determinations of the three
Figure 12. Orbitals in the molecule C2H4.
A-I Atomic and molecular orbitals
383
hybrid orbitals with respect to the sp2 hybridisation :
Tetragonal hybridisation This state draws on all states without exclusion through a hybridisation which corresponds to the structure of diamond and is further detailed below.
Sp3
2 sp3 Hybridisation a Rotational symmetry of the orbitals The normalised wavefunctions for the s- and p-states (with r ~ rf) of the valence electrons in carbon (n = 2) result from initial calculations (see Section 1-1): Is) = R n,o(r)80,o¢o = h(rrJ = S IPz) =
~2'1; IIR(rr) cos e = g(r) cos e
= zf(r) = Z =
(n = 2, 1 = 0, m = 0)
(n = 2, 1= 1, m = 0)
~2'1; IIR(rr) sin ecos
= g(r)sinElcos
(n = 2 , I = I , ill = I)
~2'1; IIR (rr) sin osin
= gtrj sin Osin c = yf(r) = Y =
(n = 2, 1 = I , m = -I)
(the functions fer) and g(r) are related simply by g(r) = rf'(rj) . The four proper functions, S, X, Y and Z constitute the orthonormalised basis for a space in four dimensions. On considering the carbon hybrid state sp3 in which none of the four orbitals (X, Y, Z and S) playa specific role, the proper functions of this new state can be developed using the preceding basis, although we now have four more functions to deal with given the number of dimensions in the system; lll i =CltS+alX+blY+CIZ
j
1lI2 = Cl2S + a2X + b2Y + C2Z 1lI3 = Cl3S + a3X + bj Y + C3Z 1lI4 = Cl4S + U4X + baY + C4Z
384
Optoelectronics of molecules and polymers z
x
Figure 13. Representation of IlJj .
IWI} , IW2}, IW3} and IW4} are the hybrid orbitals which correspond to the excitation 1s22s22p2 --+ 1s22t4. This is only possible if the reached energetic states are equal to the gain in energy required by the atomic excitation. Here m is the unit vector going in the direction and the point M has the spherical co-ordinates rr, eand <poIn Cartesian co-ordinates ex, ey and e z are the unit vectors for ----+
.
the axes Ox, Oy, Oz, and the respective components of OM are x = rf sin e. cos
e
Given the form of X, Y and Z, detailed at the beginning of this Section, we can write : x = g (r) . ~x . ~ Y = g(r) . ey . m Z = g(r) . z .
[
e m
We can now write (with i = 1,2,3,4): Wi = ajS + g(r) (aje x + bjey + cje z) . m. On introducing the vector tj = aiex + bjey + Cjez , which thus has components ai, b., and Cj in the system based on the axes Ox, Oy, Oz. Each function Wj can now be written as: Wi = cqS + g(r)tj . m. With Iml = I, Itil = Jar
+ br + cr and on setting co =
(tj, m), we have
We can state that Wj = ajS + ~j , in which the orbital ~j thus introduced exhibits the form ~j = a.X + b.Y + CjZ = g(r)tj . m. Once ~i is normalised co-linearly to ~i, and by consequence verifies: ( ~i1 ~ i) = 1 and ~j = A.j~j.
A-I Atomic and molecular orbitals 385 ~i
thus takes on the form
~i
-, -, ---+ ---+-, = g(r)ti . m = g(r) cosu], m) = 00 . m, in which OD = g(r)t j •
= (t~ , m), now ~i = OD cos 00, the position of points M' are such that ---+ ~j = OM' is a sphere with diameter 1001 = g(r) and is directed following the unit vector ti . Figure 14 shows, in the plane of the paper, a representation close to that which allowed us to determine the pz orbitals. Similarly, the M points are placed so that OM = ~i = Ai~I giving rise to a sphere of radius Ai 00. As in Figure 13, we finally reach the hybrid orbital Wi through the addition of the S orbital (which has a spherical symmetry around 0, as shown in the Figure) with the orbital ~i = Ai~i, and is also equivalent to a rotation about t~ or about ti(= Ait~). Using
00
-,
b The angle between the direction of equivalent hybrid orbitals It is possible to determine the expression for the angle between the directions for two orbitals of the ~j (or ~i) type in rotation (so that the WI and W2 orbitals are equivalent). z
o '*_-'---_~L.-.y
x
.........
Figure 14. Representation of
386 Optoelectronics of molecules andpolymers If we take the indice of the two orbitals under consideration using eqns (I) and (2), we can write, for example, IIII
= (XIS +;1 = (XIS +
W2
AI~I
= (XI(S +
J.LI~I)with
AI
= (XtJ.Lt;
= (X2(S +
J.L2~2)with
A2
= (X2J.L2.
= (X2 S +;2 = (X2S +
A2~2
The orthogonal addition of IlII and 1lI2 gives: (1lI111lI2)
= (XI(X2(S + J.LI~I IS + J.L2~2) = (XI(X2[l + J.LIJ.L2(~11~2)] =
°
(with the functions S and ~i orthonormal with respect to one another). With (XI and (X2 unequal to zero, we can say that we should have 1 + J.LI J.L2 cos (X12 = 0, in which (Xl2 = ct~, t~) represents the angle between the two directions given by the rotational axes ofthe two normalised wavefunctions ~l and ~2. The interchangeability of orbitals applied to the orbitals IIII and 1lI2 in effect impose that J.L I = J.L2 (Ill I and 1lI2 orbitals, as for S orbitals, are equivalent as the parenthesis has the same coefficient of I, and so we should have J.L t = J.L2 = J.L so that III t == 1lI2). Finally, we can state the orbitals III t and 1lI2 are equivalent if cos (X l2 = - ~. fL
c Wavefunctions in the sp3 hybridisation
Here we now have a carbon atom at the centre of a tetrahedral with orbitals about axes that join the centre to the extremities of the tetrahedron, as shown in Figure 15. The lines of the axes have angles between them which can be calculated, for example, using the t~ and t~ components. As It~ I = 1 and the carbon is at the centre of a tetrahedron, we should be able . that a'j 2 + b'12 + c,j 2 = 1 and a' i other terms that a' = to wnte a l = b'I = c,I' and ill at a, b~ = c~ = ~. Similarly, for t~, and in taking into account its geometrical position, , , I db' I a2 = c2 = J3 an 2 = - J3' From this we now have cos (X l2 = t~ . t~ = that is (X l2 = 109°28' and - ~ =
-1,
-1, which is the same as writing J.L = ../3.
Figure 15. sp3 Hybridisation.
A-I Atomic and molecular orbitals
387
Using \lJ] = aleS + Itl~]), we can say that \lJ, = al(S + J3~I) , and the normalisation condition for \lJ I brings us to a value for a I:
Finally,
in which (ai, b'l' ci) are the director cosinus : ai = bi = c', = ~ , to yield :
We obtain :
\lJj = 1(S +
1
\lJ4 = 1(S -
+Y -
Z)
A-2
Representation of states in a chain of atoms
I A chain of atoms exhibiting a-orbital overlapping 1 o-orbitals and a compliment to the exampleof 8 atoms in a chain A chain of 8 atoms (N = 8) was detai led in practical terms in Chapter I, Section VII. Each atoms presented was considered as having the s state . The energy levels are shown in Figure 1-24 and the repre sentative functions for the lowest lying band bonding states (of the function 11114 ) and the highest band antibonding states (of the function 1111<0) are shown explicitly in Figures 1-22 and 1-23, respectively. Figures I-a and l -b describe the forms of these func tions as an aide -memoire. In addition , between k = leo and k = k.t there are the intermediate states, which are represented the real parts of the wavefunctions III~ I and 1II~2 for k = kl in Figure 2 and for k = k2 in Figure 3, with 8
L cos(kpta)wo(x -
lII~p (x) = R (lIIkp(x) = Co
ta).
1=0
Here, I
Co = -
(2:
P
VN' kp =
2n: Na
and
1II0(x - ta) = Ce- crx •
For p = I, we have: n:
k, = -
4a
and
2n: Al = - = 8a. kl
The successive values for t, k , ta = ~ t, and cos ~ t are listed in the table below. 2
3
4
n
rt
4
2
3n: 4
rt
0=8 k jta
= n
cos - t 4
n: 4"t
0
.,fi
-
2
= 0.707
5 5n: 4
6
7
3n: 7n: 2
4
0 -0.707 - I -0.707 0 0.707
390
Optoelectronics of molecules and polymers
........ljlss"i.(jlso
(a)
.----+-----.----+-----.---...... --____4~-- .......--____4I~___+x I L=Nd
1...
..;(j
::iji;.j
~·i···· ·· · · ·:·ip;j· · · · · · ··· · · · · ·iP.
::..ip;;
iji;.··········:··ip;;·············ip;i ;;iji;o····· (b)
Figure 1. (a) Representation of IJlko =
\IJ~I = \PsO",8 + 0,707 . \PsI - \Ps4 -
+ 0 . \Ps2 - 0,707 . \Ps3 0,707 . \Ps5 + 0 . \Ps6 + 0,707 . \Ps7
We can thu s see that when k = k j, the nodal points start to appear in the wavefunct ion as shown in Figure 2.
.----------,::>"""''''"---..., "
,,
,,
I
,,
I
I I
,
,/
'" ........... ....
1.., = 8a
_--
__ I
I
..
;'
"
Figure 2. Representation of IJIkl with IJIkl = Re(lJIkl) =
+ 0 .
A-2 Representation of states in a chain of atoms
391
- For p = 2, we have
Jt k2 = - , 2a
and
2Jt ).2 = TI = 4d 2a"
The successive values of t, k Ita = I t, and cos I t are shown in the table below:
0=8 kjta =
I 2
3
4
5
6
7
Jt Jt 3Jt 5Jt 7Jt 0 = 4Jt - Jt - 2Jt - 3Jt 2 2 2 2 2
-t
o -1
0
o
Here we can state that at the centre of the band, for k boding nor antibonding, as shown in Figure 3.
- I 0
= k2, the states are neither
2 General representation of states in a chain of overlapping (J s-orbitals When we have positive s-orbitals (a lone, single atom with an s state-see Appendix 1-4, Figure 4) and a chain as in Chapter I, Section VII, we have from Chapter I, eqn (20) -
~ s = N/o(x - ta j] W(x - sa) l\{Io(x - sa)} = (\{It I W I\{Is) < 0, as \{It and \{Is have the same positive sign (from the orbital of the lone nOt or nOs atoms) while W < 0.
From an energetic point of view, the result with E given by eqn (22) of Chapter I that E, = Eos - a s - 2~ s cos ka, and the energy is, as in the lower half of Figure 4 for s-orbitals:
k
A=4a
<:..fi"~5·-·· -·---·--~··]'"'--·--····· -1s".::.::.::.
'\1 I V ...............
Figure 3. Representation of 1lJ~2 with 1lJ~2 4ls4 + o· 4ls5 -- 4ls6 + 0 . 4ls7 ·
....i.4-Re(expiikjta)
...........
= Re(llJk2) = !PsO~8 + O· !Psi -
4ls2 + o· 4ls3
+
392
Optoelectronics of molecules and polymers E
.--.-........' - 2~""
E~ ~O'*-Pb~d
- p band E~--f"2jtaP--j
,
-Ebs--t-
i
Os
- 1tia
;
!
;
0' -
Os -
t
Msban1 t s- - -
* - s barid
,
I
2~s
i
rita
Figure 4. E = f(k) curves for the a overlapping of sand p orbitals.
•
•
lowered at the lowest part of the band as -~s is always negative and cos ka > O(-rr./2 ::::: ka ::::: rr./2 at the bottom of the band) and we have a bonding state (c-s band); increased at the highest part of the band as -~s is always negative and cos ka < O(n 12 : : : ka ::::: rr. at the top of the band) and we have an antibonding state (o'*-s band).
This result can again be found by taking into account the phase term associated with each wavefunction for each atom in the chain : •
•
two adjacent and bonding s-orbitals are in phase (k = 0 as in Figure l-a) and have the same sign . The geometrical form and the orbital and its sign can also be shown graphically, as in Figure 5-a. The interaction (coupling) of the two states gives rise to a decrease in the energy (the o-s band); however, the antibonding states are associated with adjacent orbitals which have opposite phases (when k = ±rr./a) and also therefore opposing signs, as in Figure l-b. This situation is represented in Figure 5-b in which the geometric form of the orbitals along with their signs are shown . The energy resulting from their interaction is increased (in an unfavourable state) and the result is the (0'* -s band shown in Figure 4.
(aJ~
k =0
(bJ~------+e------~@------ie--------t@
k = rda
Figure 5. Distribution of: (a) a-s bonding orbitals; and (b) o"-s antibonding orbitals (arrows indicate phase terms).
A-2 Representation of states in a chain of atoms (a)
00
393
-~------ -~-------~-~ x -~----- --~----- - -~-~
Figure 6. Distribution of: (a) antibonding 0 * -p orbitals; and (b) bonding c- p orbitals (arrows indicate phase terms).
3 General representation of states in a chain of overlapping cr p-orbitals For the p-orbitals, once again we can use -~ap = (\Ilo(x - ta) IW(x - saj ] \I1o(x - sa) ) = (\IltlW I\Il s ) where W < O. Now the functions \Ill and \Ils represent p-orbitals, which have the form shown in Figure 6. Noticeably each has adjacent positive and negative lobe s so that -~ap is positive (see the upper half of Figure 4 which details a-p orbitals). We can note that: •
when -n /2
:s ka :s n /2 , cos ka >
Ctp ;
•
when n/2 :s ka :s nand -n :s ka decreases by E~p = Eop - Ctp.
0 and the energy is increased by E~p = Eop -
:s -n /2, we have co s ka <
0 and the energy
The same result can be found : •
•
when k = 0, the wavefunctions are distributed in phase (following Floquet' s calculations, the term cos kpsa is equal to I ) and they can be geometrically represented as shown in Figure 6-a (using as example the px-orbital s). A positive lobe interacts with a negati ve lobe to produce an antibonding state with the appropriate increase in energy (o"-p band shown in Figure 4). Thi s beha viour is in opposition to that of the s band in the same k region; or when k = ±n/a, the phase factors altern ate (cos kpsa equ als, alternatively, + I and - I) so that the geometric repre sent ation is that shown in Figure 6-b and corresponds to the interaction s between lobes of the same sign. The result is a decrease in the energy for what is a o-p bonding state as detailed in Figure 4.
II n Type overlapping of p-orbitals in a chain of atoms: n-p- and n*-p-orbitals The pz-orbitals bonded to each other by a n -bond give rise to a n - p type orbital, as shown in Figure 7. The resonance integral , -~ llP ' involves both the overlapping of the two positive and the two negati ve lobe s. With W < 0, -~ Jtp is now negati ve (as for - ~s) giving a behaviour similar to that of (a -s-bonds . Figure 8-a and -b show, respecti vely, the geometrical representation s of the lowest energy bonding and highe st energy anti-bonding orbitals.
394
Optoelectronics of molecules and polymers
z
Figure 7. The rr-p-orbital,
(a)
(b)
Figure 8. Distribution of (a) n- p-orbitals and (b) rr"-p-antibonding orbitals.
III
(J-S-
and o-p-bonds in chains of atoms
In general terms, and as we have seen in Chapter I, with k = n j a a stationary wave system can easily arise. The wavefunctions and the presence probabilities take up solutions of the type (Figure 1-5) in which: • •
the electron charges are esse ntially spread in the neighbourhood around the lattice nodes, so that \11+ ex: cos( n xja) and p+ = cos 2( nxja); and the charges are essentially about the mid-point between lattice nodes, so that \11- ex: sin( nxja) and P- = sin2( n xja) .
Given the geometri cal shape of the atomic s- and p-orbitals and their corresponding electron distribution s: • •
the electron charge s associated with s-orbitals are concentrated about the atomic nodes with probability p+ ; and the concentration of electrons associated with px-orbital s, mid-way between atomic nodes, can be expressed as the probability P- .
In terms of energy the two orbitals and their associated electron concentrations are separated by a gap of EG which is precisely defined by k = n j a. In addition, as the waves (\11+) associated with the s-states tend to concentrate electrons in the neighbourh ood of the centre of the atoms, the electrostatic interaction energy effectively lowers the energy of the electrons, which are more stable than
A-2 Representation of states in a chain of atoms
395
those associated with the progressive wave (in exp(ikx)) which delocalises any sort of electron. Conversely, the \11- wave associated with the p-states concentrates electrons at the mid-point between atoms (that is the further point from the centre of the atoms involved) and minimises as much as possible the electrostatic interaction energy. The result is that the electron charges are less stable than those associated with a progressive wave (in exp(ikx) delocalising all electrons) of the s-states \11+ wave. Thus, in this particular example, an energy gap can appear in a I-dimensional system with the simultaneous existence of at least two orbitals (here sand p). Figure 4 can be compared with Figure 1-12.
IV Comments 1 The Bloch function In Chapter I it was shown how with a zero order approximation (an electron placed in a flat-bottomed well) an electronic wavefunction can be written: \11k (x) = \110 = e ikx
(to the order of a normalisation constant).
However, for a semi-free electron (placed within a potential well with a bottom perturbed by electrostatic interactions with atomic nuclei situated at lattice nodes and x) we need to find a wavefuncundergoing a periodic perturbation w(x) = wo cos tion for the perturbed state of the type \11k (x) = \I1ou(x) = eikxu(x), in which u(x) is the unknown function . With a potential perturbation of w(x) , the Hamiltonian can be written as 2 d H= dx 2 + w(x) ,
2;
-n.
and is conserved on undergoing the translational operator Ta, which transforms x into x + a. This can be expressed in TaH =
_n.2 d(x +d a) 2 + w(x + a) = -n2 -dxd 2 + w(x) =
H.
H remains invariant with respect to the effect ofTa, and commutes with Ta: [H, Tal = O. We can thus find the same proper system of functions for T, and for H, in a process which is followed up in most standard text books on quantum mechanics. In order to find the form of the proper functions of Ta which can also be taken as the proper function of H, we can use the following equation which they verify :
The product from the application of these functions is T a 0 T - a, and involves successive translations with modules -a and then a so that the operator T, 0 T - a changes
396
Optoelectronics of molecules and polymers
as though it has the identity I. Thus:
From this we can deduce that Ck,aCk, -a the proper values becomes:
= I, that is Ck,a = eika, and the equation for (1)
From outside we have the definition of the operator Ta which transforms x to x + a, and allows the expression:
(2) On comparing, eqns (1) and (2) we can extract u(x) = u(x + a). So, the proper function Wk (x) = eikxu(x), which describes the state of a semi -free electron-which has the form under analysis-is such that u(x) = u(x + a). This proper function, Wk(X) = eikxu(x) with u(x) = u(x + a) is called the Bloch function.
2 Expression for the effective mass (m") By definition, m * = Fex! , in which y = ~ and vg, in the dualistic theory, is given by the velocity of the package of the wave group as dw
vg
= dk '
so with E = lu»,
IdE
vg - lidk'
and
Yg
=
ld (dE) lidt dk
2E
=
Id dk Iidk 2 dt .
In addition the exterior work force (Fext = qE ext for an external field Eext applied on a charge q) is such that dE = Fextdr = Fextvgdt, so F
ext
=
IdE vgdt
=
IdE dk vgdk dt
=
d~ dE dk dk dk dt
= Ii dk . dt
Calculating the ratio Fext
Y
2
. * 1i = m* grves m = d2E' (jj(2
For a free electron, E
= n;~2 , and we find again m = m* as Fint = 0, so that Fext
= FTotal = my = m*y .
A-3
Electronic and optical properties of fullerene-C60 in the solid (film) state
I Electronic properties of fullerene-C60: the band scheme as indicated by the Local Density Approximation Method [Tro 92 and 96] Figure I schematises the first Brillouin zone of the cubic face centred (cfc) system of fullerene-60 (C60) . Table I goes on to detail the energies of states at the centre (I') of the Brillouin zone and have been calculated using the density function in the Local Density Approximation (LDA) [Tro 92]. In Figures 2-a and -b the theoretical state densities are compared against empirically obtained photoemission or inverse photoemission spectra, respectively. In Figure 2-a, the theoretically obtained spectra of the density of full states, compared against photoemission spectra, and the highest energy peak arising from a valence band results from the TIs-states. These states are derived from the HOMO h u k,
x
ere
Figure 1. Brillouin zone for a efe structure.
398
Optoelectronics of molec ules and polymers
Table 1. Electronic state energies for C60 at the Brillouin zone point
r.
Energy (eV)
Labe l
Energy (eV)
Labe l
Energy (eV)
Labe l
-18.766 - 18.146 - 17.262 - 17.22 1 - 16.098 -15.381 -15.326 -14.137 -13.983 -13.585 -13.542 -12.021 -11.993 - 11.873 -10.91 7 - 9.830 -9.752 -9.564 - 9.423 - 8.252 - 8.128 - 7.368 -7.271 -7.114
aO-ag a , -tu a2- tg
-7.109 - 6.533 - 5.829 - 5.802 -5.563 -5.389 -5.371 -5.257 -5.004 -4.946 - 4.929 -4.587 - 4.109 -4.089 - 3.597 - 3.452 - 3.189 -3.120 -2.766 -2.755 -2.628 -1 .850 - 1.615 -1.084
a7- tu a7- tu a7- au a7- tu IT,-tu
-0.965 -0.225 0.000 1.710 2.372 3.469 4.052 4.103 4.217 4.971 5.149 5.515 5.878 6.240 6.423 6.495 6.974 7.212 7.430 7.454 7.815 8.298 8.318 8.754
1q -tg
a2-eg a3- tu a3- au a3- tu a4-eg a4-tg a4- ag a4-tg as-eu as-tu as- tu as-tu a6-tg a6-eg a6- tg a6-ag a6- ag a6-tg a7-eu a7-tu ITO-ag
IT2-tg as-eg as-tg IT2-eg as-ag as-tg as-tg ag-tu ag-au IT3-au IT3-tu as-eg as-t g ag-eu ag-tu IT3-tu IT4-eg IT4-ag IT4-tg
ITS-eu ITs- tu ITs-tu IT6-tg ITs-tu IT6-eg IT6-tg Co-ag IT7-eu IT6-ag IT7-tu ag-au IT6-tg ag-tu OO-ag TOA-au TOB -ag C, -tu alO-tg ag-tu C2- tg alO-eg O,-tu
level of the molecule, which is however broken down on the interior of the tetrahedral crystal to give 5 bands with symmetries tu and e u. Yet this dispersion of bands does not permit their resolution and the breakdown can only be discerned at the point r (see Table I) . In the same Figure 2-a, the band of TI4 -states derived from the molecular states gg and hg. On increasing the energy of the bond , there is the first appearance of (J and TI charac ter mixtures. In Figure 2-b, the theore tical spectral state dens ities calculated for empty states are compared against inverse photoemission spectra. The conduction band, here called 'A', is formed from TIS states, which are derived from LUMO states exhibiting T,u symme try. There follows this the band ' 8 ' formed from TI6-states and appears at an energy lower at the point r than in the state densi ty spectrum. On dissecting the various contributions which go up to make the 'C' band, it is possible to see that the first non-mo lecular state is at 4.217 eV. This state and its wavefunction are localised about the centre of the molecules and, characterised by L = 0, is denoted Co.
A-3 Electronic and optical propertiesof fullerene-C60 in the solid (film) state
E,=3225 eV
....'"
'" .:!:!
'tl
=
-e
....t'l .... rJ:J
.... .... rJ:J
,~
399
b
.<;:
';;
'" =
~
~
~
~
~
-20
-10
Energy (eV)
o
o
10
Energy (eV)
Figure 2. (a) Calculatedstate density functionsfor the valenceband and empirical photoemission spectra. The lower 2 plots show density distributions for (J and IT at I'd of the Brillouin zone (bands numbered in terms of L); and (b) the lower conduction band function densities compared against two experimentally obtained inversephotoemission spectra.
Using the self-consistent field theory it was shown that there are relatively flat regions at the centre of the C60 sphere and in the tetrahedral and octahedral interstitial sites of a cfc lattice. The wavefunctions localised around these sites appear with energies between 4.8 and 5.3 eV above the conduction band and are called 00, TOA and TOB, with the latter two names being, respectively, for bonds and antibonds around a tetrahedral site. The D and E peaks are due to simultaneous contributions from both molecular and non-molecular states; in effect they have reached the stage of delocalised states . We can see that with these results the derived peaks are distinct, considerably more so than those observed for graphite and diamond and would tend to indicate the molecular nature of solid C60. As already discussed in Chapter Ill, we can safely say that Hiickel's method results in a good approximation. To end this Section, we have shown the structure of the C60 crystal bands along the ~ senses in Figure 3. They are defined by the points r and X from the Brillouin zone and Z defined by X and W, as shown in Figure I. Figure 3 shows energies close to the fundamental gap and shows the highest group of valence bands and the two lowest groups of conduction bands . The direct gap is here determined as 1.2 eV at the point X, although this method tends to underestimate the actual value .
400
Optoelectronics of molecules and polymers
---=::
3.0
-.
1T6~ 2.0
:>
1T,
Col '-'
~
"-
LO
Col
C
W 0.0
:>:<
1T,
~ -LO
r
x
z w
Fig ure 3. Band structure of C60 in a cfc structure along the 6. and Z directions .
t 1u
'i ·· ·:,,v
LUMO
·, ,
HOMO
(b)
Figure 4. (a) The relationship between the experimentalI y derived state densities in the solid and the molecular orbitals levels along with permitted transitions [Law 92]; and (b) permitted transition s derived from the energy levels of molecular orbitals. The v band is forbidden for reason of symmetry, however, it is not excluded from electron-phonon coupling effects and appears weakly in the spectrum [KeI92].
A-3 Electronicand optical properties of fullerene-C60 in the solid (film)state
401
II Optical properties and observed transitions It has been observed that the absorption spectra derived from solid C60 were very close to those of C60 in the molecular state , a result which indicated that C60 displays only very few interactions between molecules in the solid state [KeI92] . The eventual similarity of spectra derived from solid and solution state C60 allowed an attribution of the solid phase bands, along with help from known optical transitions associated with the energy diagram of molecular orbitals as shown in Figure 4-a. Even though the h u ~ tl u transition is forbidden, (as it accords t.L = 0 and not t.L = ±I-see Figure III-I 3 where the h u and tl u levels both correspond to L = 5), it is nevertheless just observable (Figure 4-b) . This is due to vibronic coupling which modifies the selection rule (see Chapter VII on optical properties for further details). And accordingly a rather weak band at 550 nm (2.50 eV) was attributed to this transition [Law 92] with an energy rather elevated when compared to alternative estimations (from 1.5 to 1.9 eV). Figure 4-a permits the deduction of the energy of additional transitions which are h u ~ tl g, hg ~ tl u, h u ~ hg, gg ~ t2u , and h g ~ t2u,each of which has, respectively, an energy of 3.0, 3.4, 4.3, 5.0 and 5.4 eY. The se values coincide quite closely to those experimentally derived [Kel 92].
A-4
General theory of conductivity for a regular lattice: the Kubo - Greenwood equation for conductivity in delocalised states and expressions for mobility
I Electron transport effected by an external force and its study 1 Effect of force on electron movement and reasoning within reciprocal space Here we take as example a square plane crystal with sides (L) defined by L = na. The Brillouin first zone and the dispersion curve (E(k)) exhibit the forms represented in Figure I . The first band is assumed to be partially occupied by electrons in a symmetrical manner so that E(k) = E( -k). At the point of thermal equilibrium, the velocity of an electron can be given by :
_ l~ v = -gradkE. Ii
(I)
As all the carrier velocities cancel each other out (orthogonal in the circle E = constant as in Figure l-a) the total result is zero and there is no charge tran sport.
E
- rc/a;;-l--I-'--t--+-+-~·kx
- rc/a - rc/a
rc/a
Figure1. Representation of a reciprocallattice with: (a) the Brillouin zone and an equi-energy surface; and (b) the dispersioncurve E = f(kx ).
404
Optoelectronics of molecules and polymers
Comment Eqn (1) can be justified by the following: the velocity of an electron can be repre sented by the velocity of the group associated with the wave packet, which describes the wave-like character of an electron: I aE
aw
with E
= lu» ==:} vg = h ak '
I ----+ _ vg = hgradkE = v
(simplified notation ).
vg -' - ak' to give in 3-D:
If an external force (F) is applied for a certain time (dt) on an electron which has a velocity then the resulting change in energy is expressed by dE = F. dt.
v,
v.
Following eqn (1) we have: dE = Additionally, in 3-dimensions
F(kgradkE) dt.
By identifying between the two last equations,
-
dk
F=n-. dt
-
(2)
-
Eqn (2) shows how F and dk are colinear and result s from the e!fect of a force displacing an electronic population in the Brillouin zone parallel to F (dashed circle in Figure I) , and the distribution symmetry is perturbed (as E(-k) =1= E(k)) . The resulting speed of the electrons is non-zero and charge transport is initiated .
2 Boltzmann's transport equation At the thermodynamic equilibrium, the probability that an electron with a wave vector k will be in the reciprocal space is given by the Fermi-Dirac function:
fo(k) =
I ~ 1 + e(E(k)-EF) /kT
(3)
This function changes in the presence of an external force: f (k, r, t)
= fo(k) + fl (k , r, t)
(4)
Most generally, this function depend s not only on k but also on the geometrical position (r) of an electron, when the force induce s a local inhomogeneity in temperature or concentration, and also on the time (t), if the permanent regime is not reached. During an interval of time dt, the variation in f is equal to the sum of variation s caused by the applied force (interactions with the exterior) along with a contribution
A-4 General theoryof conductivity for a regularlattice
405
due to collisions (internal interactions). This gives:
M(M) = dt
dt
applied force
+
(M) dt
collisions
And with (df)rorces
= (Oinstantt-dt -
(Oinstantt
f(k~ ~r) - f ,
(~dk k - -dt ~r -
I
=-
= -[(Oinstantt -
dt
dr ) -dt dt
'
I
(Oinstantt-dd
of = - -dk ok
of -dr
or'
during the interval [t - dt, t] we have: df ) of dk ( dt forces = - ok dt
-
of dr or dt '
and in 3-dimensions: -
dt
dk
-+ (fr - grad.f . -
dt
dt
-+ = -gradkf . -
df )
(
forces
On introducing the last expression into eqn (2) and given that df ) (dt
(r, k)
-+ = -n- l~F · gradj f -
v=
-+
~~, we find:
~-+
v . grad.f
Applied force
With respect to the collisions, the contribution is in the following form (system with a relaxation time): (
df ) = _ f - fo, dt collisions t
*
t
being the relaxation time .
Under a permanent regime, is zero and we find Boltzmann's equation (in which we have replaced f by fo for all gradj f and grad, f , in a legitimate act as fl « fo and the perturbation is weak and therefore negligible with respect to the value at the equilibrium state). I~
-+
~
-+
Ie F · gradj fo + v . grad, fo +
°
.
-+ homogeneous, then grad.fi, = 0, and
r
If we assume that the crystal we have eqn (5) becomes -+ n- I~F · gradkfo + -fl t
=
f
-l
IS
(Boltzmann 's equation).
I~ -+ = 0, or even f, = -tli- F· grad; fo
(5)
(5')
On taking the latest expression and inserting it into eqn (4) f = fo + f], and on using eqn (I) for velocity to finally obtain
v = *grndkE, we can write that grndk fo = ~gradkE = n~~ v, f = fo -
t .
~
~
ofo
F.v. ClE
(6)
406
Optoelectronics of molecules and polymers
II State density function, carrier flux and current density in the reciprocal space 1 General expressions for fluxes of particles The flux of charge carriers generated by an applied force (F) is consi stent with respect to the product of the concentration (c) of charge carriers of a certain charge (q) and their displacement velocity (Vct). This is because the flux repre sents the quantity of charge which traverses a unit surface in a unit time. So we can write for the average over all carriers that (<1» = (cqVct ). In reciprocal space , the carrier concentration is expressed by c = Jk N(k)f(k)d 3k, in which N(k) is the state density function and repre sents the number of possible states for carriers in a unit volume in reciprocal space when they are in a unit volume in direct space . We can thus write that <1>
=
1
N(k)f(k)q(k)v(k)d 3k .
(7)
2 Expressions for the state density function a Initial comment on the expression for charge carrier concentration From the expression we have just given for the state density function N(k) in reciprocal space, we can directly note the carrier concentration by: n=
1
N(k)f(k)d 3k , so with f
~ fo, n ~
1
N(k)fo(k)d 3k .
(8)
b Form of the state density function in k space In order to evaluate N(k), we can use a simple cubic lattice with sides of length L. Here the conditions on the periodic limits (the Born-Von Karman conditions) are written , for example, in the x direction so that 1\J(x) = 1\J(x + L) and are applied to the Bloch wavefunctions, as in: \IJ(x) = eikxu(x) = 1\J(x + L) = eik(x+L)u(x + L) [with u(x + L) = u(x) as L is written as L = na in which a is the crystal periodicity] . This gives us the relationship e ikL = I which fixes the form of k, which has to be such that k = n (where n can be either positive or negative) . In the direction kx, one cell (the space in which we can place a state without which can having to take spin into account) therefore has the dimensions ~kx = be written in 3-dimensions, using the usual notations, as (~k)3 = 8~3 (with V = L 3).
22
22 ,
Without taking spin into account, the number of states into which we can possibly place carriers, in a unit of reciprocal space, is equal to (~~)3 = ~ . Once we introduce the spin states, which multipl y by two the preceding result, and remember that N(k) is defined for a unit volume of direct space (V = 1), then
A-4 General theory of conductivity for a regular lattice
407
we can write definitively the density function of N(k) states as: N(k) = 2 ( V3 ) 8n
V= l
I 4n 3 ·
(9)
c State density function in energy space The titled function we shall denot e as N(E) , although sometimes it is called Z(E), and it such that N(E)dE repre sents the number of states distributed in energ y space between E and E + dE, the whole still being in respect of the direct unit volume in space (V = I). Supposing that the electron effecti ve mass (m" ) is invariable whatever the value of k, and that variations in k are isotropic in the space of wavefunctions, then we can write (in approximation of the effective mass) that E =
~~: , taken with p = lik = nr'v,
E = 1m*v2 (and thus with v = ~~). In k space, as shown in Figure 2, the surface equienergy E = cte, and is a sphere of radiu s k = with radiu s
¥. In the same way the surface of the equienergy E + dE is a sphere 2
k+dk=
,J2m*(E + dE ) ( li (k + dk)2) asE+dE= . Ii 2m*
In term s of the state density function , the densit y of the states N(E)dE corresponds to the density of states spread throu ghout the k space in between the spheres of radius k (for E = constant ) and k + dk (where E + dE = constant). As the volume held between these two spheres, and shown as the greyed zone in Figure 2, is equal to d 3k = 4nk 2dk , we can write that
N(E)dE = N(k)d3k . With 3
d k =4n
(2m*E) 1/2 m*dE . - 2- ' Ii Ii
we have:
Figure 2. Representation of equi-energy spaces within reciprocal space.
(10)
408
Optoelectronics of molecules and polymers
From this we deduce that (11)
3 Expression for flux In general terms, eqn (7) describes the carrier flux and is an expression in which we can now introduce the value of N(k) given by eqn (9). Additionally, the statistical distribution function (f) is such that f(k) = fo(k) + fl (k) and with the velocities being zero at the point of thermodynamic equilibrium it is only f 1(k) which contributes to the expression for the carrier flux, which can thus be written: (7')
4 Expression for current density in reciprocal space For a force due to an applied electric field we can assume that the electric field (Ex) is applied parallel to the axis k, in reciprocal space in order to simplify the expressions used. With the force being exerted on a charge q being F(x) = qE x, eqn (6) becomes
afo f = fo- q"[Exvx as
(6')
On writing E - EF)]-I = [u(E)r 1 and posing v = (E - EF) , fo = [ 1 + exp ( ~ ~ the derivative with respect to E in the expression for fo gives :
2' .with · u' = [1 + exp(v)] , -afo = - [u(E)] -2 u' = -fOll aE 1 exp(v). = [exp(v)] " = v exp(v) = kT
As I
+ expv =
I I - fo , 1 I - fo -, soexp(v) = - - , we have II = - - fo fo kT fo
and finally :
afo fJ 1 - fo fo = - - - - = --(1 - fo) aE kT fo kT
(12)
We then find that eqn (6) gives f = fo + for-rExvx(1 - fo), in which f - fo = f1 = r-rExvxfo(1 - fo)·
A-4 General theory of conductivity for a regular lattice
409
On assuming that the field Ex is constant and uniform, the result gained from eqn (7') for the flux, now the current density (Jx) is such that:
(13) (Here the Boltzmann constant is denoted kB in order to distinguish it from the wavenumber k which defines the reciprocal lattice and is such that, for a cubic 3-dimensional system, k =
Jk~ + k~ + k~.)
III Different expressions for the current density and relaxation times and forms of conductivities and mobilities 1 Usual expression for current density in energy space Eqn (13) which gives the current density can be rewritten as a function of energy by using eqn (10), which is such that N(E)dE = 4~3 d 3k . Eqns (7) and (13) thus give : 2
Jx = q Ex
~
E
-rv2x -fo(l - fo)N(E)dE . kT
(14)
When considering both an isotropic diffusion and the approximation for the effective 2) 2 = VY 2 = vz2» (iIn W hiICh V2x = "3 V 2 = 3m*' 2E Inserting . m*v an d vx mass th en E = -2,so t h at vx this value for v~ into eqn (14) in addition to eqn (11) for N(E), and on setting A = ~~ (2m*)3 /2 we now have J x = -2 ; 2Ex 34)"[ m*kT
f
In addition, from eqn (8) we have n ~
-r(E)Efo(l - fo)AE 1/ 2dE .
fk
(14')
N(k)fo(k)d 3k, that is:
in which
(8') Introducing eqn (8') into eqn (14') results in Emax
J _ ~ nq 2Ex fo x - 3 m*kT
-r(E)E 3/ 2fo(l - fo)dE foEmax El / 2fodE .
(15)
410 Optoelectronics of molecules and polymers 2 Studies using various examples a When
is a constant i.e. T(E) = T
T
"[ can be given by the integral I of a numerator which is limited: 1= IoEmax E3/ 2foO - fo)dE. On using eqn (2): 1= -kT
r-
10
E
3
/
3 2 max 2 afo aE dE = -kT {[foE / JE
0 - 10[E
max
3 l/2fodE} . 2E
The first term in the integration by parts is zero (as fo(Emax) = 0 when Emax ---+ 00) , so that I = ~ kT IoEmaxE1/2fOdE. Moving this into eqn (5), we find the usual formula nq2"[ Jx = --Ex .
(6)
m*
b Degenerate semiconductor C'L First order calculation Here the Fermi-Dirac function goes from I to 0 in small intervals (of the order of kT) about EF. So for E < (EF - kT/ 2) we have fo ~ I , and for E > EF + kT/ 2 we have fo ~ O. On placing = "[(E)E 3/ 2, for a numerator for Jx given by eqn (5) the term B appears which is such that B = k~ IoEmax (E)foO - fo)dE. Using eqn (2) and factorising the integral gives:
B= -
l
EF- kT/2
o
afo iEF+kT/2 afo i Emax afo (E)-dE (E)-dE (E)-dE. aE EF-kT/2 aE EF+kT/2 aE
As fo ~ I = a constant between 0 and EF - kT/ 2, the first term is zero, as is also the third term as fo ~ 0 between EF + kT/2 and Emax. As between EF - kT/2 and EF + kT/2, we have (E) ~ cte = (EF) , we can write
Calculating the denominator means determining [E
10
max
E1 /2fodE ~ [EFE 1/ 2dE =
10
~E~/2 . 3
(7)
On introducing the last two results into eqn (5) we have: Jx =
nq2"[(EF) m*
Ex.
(8)
A-4 General theory of conductivity for a regular lattice ~
The more generalform
Eqn (15) can be written in the form t(E)E 3/ 2fa(1 - fa)dE
nq 2E 2 I Ia
J - - -x -
m* 3
X -
411
E max
-::....::e..------;o;------kT IaEmax EI /2fadE '
so that with eqns (12) and (17) we now have 2E J = nq x [_E- 3/ 2 x m* F
[ 00 t(E)E3/2 afo dE]
ia
.
aE
By consequence (19) with
t = _E- 3/ 2 F
00
1 a
at
t(E)E3/2~dE . aE
(20)
c Non-degenerate semiconductor Here E - EF
»
2kT, so that exp([E - EF]/kT)
1 fa = I + eXP([E _ EF]/kT) in the Boltzmann distribution. As fa « 1, we have fa(1 - fa) 2
2E
J __ ~ x -
3 m*kT
~
»
1. And
~ exp([E _1 EF]/kT) = A exp ( - k~ ) fa, and eqn (15) gives :
[ 00 t(E)E 3/ 2 exp (-~) dE [ 00 E 3/ 2 exp (-~) dE kT ia 00 kT 00
ia
1
E3/2 exp ( _
k~ )
1
dE
E' /2 exp ( -
k~) dE
With
[ 00 E3/2 exp (-~) dE
{E} = io 00
1 100
{t} =
kT
32 t(E)E / exp (
[ 00
ia
k~ )
E 1/2 exp ( -
32 E / cxp
3
= -kT
dE
-~ )
and
2
dE
(E ) , - kT
dE
we finally have : nq2
Jx = -
(t) Ex . (21) m* (We can note that the weighting factor is EN(E) , with N(E) = N(E)fa ~ E 1/ 2 exp( - k~)' and not N(E) as we might initially think) .
412
Optoelectronics of molecules and polymers
3 Expressions for mobility As a preliminary step we can note that mobilit y (IL) is classically defined by one of the two relations lvl = ILEx, or a = qnu .
a When the relaxation temperature ('t (E )) is constant i.e. 't eE) nq21
Eqn (16) written as Jx = ITi*Ex allows us to write a =
~ m* ,
=r
so that
qT IL= - · m*
(22)
b For a degenerate semiconductor
a First order calculation Eqn ( 18) written Jx = ~
nq2T(Ep) m*
. nq2T (Ep) qT(Ep) Ex, yields a = , so that IL = - - . m* m*
The more general form -3 2
;: = -Ep /
00
1 o
(23)
With 8& 10 nq 2-T T(E)E 3/ 2 -dE, eqn (19) written Jx = - - Ex, aE m*
gives nq2;: a=--
m*
q't
(24)
IL = - . m*
and
c Non-degenerate semiconductor Here , eqn (2 1) written
1
00
with
(T) =
3 2 T(E)E / exp (
roo
Jo
-~ )
dE
(E ) ,
3 2 E / exp - kT
dE
is such that a = ~ m* (T), so IL =
~
m*
(T) .
(25)
A-4 General theory of conductivity for a regular lattice
413
4 The Kubo - Greenwood expression for conductivity a General case We have already realised eqn (14) for current density, that is 2
J x = q Ex
1
2
1:V x -fo(l - fo)N(E)dE . E kT
So that conductivity is in the form (J
= q
1:Vx2 -fo(l - fo)N(E)dE . kT
(26)
j..l(E)fo(l - fo)N(E)dE ,
(27)
q1:(E)v~ kT
(28)
1 L
2
E
Eqn (26) san be rewritten to give (J
= q
with j..l(E)
=
in the Kubo-Greenwood expre ssion for conductivity initially found in general physical theory . Following on from eqn (12), we can also write (J
afo(E) dE aE '
(29)
= q kT N(E)j..l(E) .
(30)
= -
[
(JE
JE
with (JE
b Isotropic diffusions and with an approximation of the effective mass 2
2 _ V ( Vx - T
2E ) = 3m"
The introduction of v~ into eqn (14) gives (J
= q [
q~fo(l
(J
= q [
q1:~fo(l
JE 3kTm* JEmtE
- fo)N(E)dE ,
-
so with E
=
3
2kT,
- fo)N(E)dE .
(31)
We once again find eqn (27) of the Kubo-Greenwood expression in (J
but here with
= q
L
j..l(E)fo(l - fo)N(E)dE,
qt E j..l(E) = - = . mOE
(32)
414
Optoelectronics of molecules and polymers
IV Complementary comments 1 Concerning the approximation of the effective mass and isotropic diffusions a Basic expressions If the band structure is known we can express E(k) as a Taylor series, as in E(k) = E(O) + k [ -aE ] ak k=O
2E]
+ -I k 2 [a-2 2
ak
+ ... k=O
Once the band exhibits a minimum at k
= 0, laEJ ak
=0
and
m*
I a2 E(k) li2~ '
E(k)
= E(O) + li
2k2
2m*
k=O
,
with
On introducing the crystal moment, lik = m*v, we have for a parabolic band which is such that E(k) - E(O) = ~~~ (which also takes into account the origin of the
i::)
energies for electrons in E(O) = Ee (lowest conduction band), E(k) = and E = im*v2. As we have already seen, for isotropic diffusions , we therefore derive
(v~) = (v~) = (v~) = ~, so that on using the effective mass approximation we have (vi) =
3;;"
b Additional remarks concerning the approximation of the effective mass [Lun 00] When an electron moves through a device, it is subject to both a periodic potential of the crystal (Vc) and an internal or applied tension (VIA) caused by impurities due to donors, acceptors, super-lattice effects and so on. Typically, VIA varies little in space with respect to Ve . Electrons evidently see both Ve and VIA. If we assume the collisions between electrons and the lattice to be negligible , then the electronic wavefunctions must accord to
2
li2 a --2 [ - 2m ax
a\IJ + Ve + VIA ] \IJ(x, t) = ili. at
(33)
In the absence of VIA, the solutions of eqn (33) are the well known Bloch functions. The question which must now be asked is with what condition is it possible to express the solutions for the complete problem as expressed in eqn (33), and, without an evident solution, do this with the help of the known forms of the simplified problem. The response is that it is possible using carriers situated at the lowest point (k = 0)
A-4 General theoryof conductivity for a regularlattice
in a parabolic band (which exhibit energy bands with a minimum at k we can write \IJ(x, t) = F(x, t) . Uk=O, in which F(x, t) is such that 2
a + VIA ] F(x, t) = -li2- [ 2 2m* ax
415
= 0) for which
aF
ih- .
(34)
at
The function \II is thus the product of a function envelop and varies slowly due to the presence of VIA in the equation, and also a function uko(r) which is periodic and varies rapidly with the Bloch function calculated from k = 0. The advantage of this type of solution is that the complicated crystal potential effects (Vc) can be written into a single value for the effective mass, hence the name the effective mass approximation. Nevertheless, writing eqn (34) did necessitate that VIA varied sufficiently slowly with respect to Ve . In effect the potential wells associated with VIA should not be too steep implicating a low level of internal disorder and tension, and a sufficiently low frequency and tension in the applied field.
2 General laws for changes in mobility with temperature a Semiconducting system (non-degenerate) We have seen that generally speaking t is dependent on the energy of the charge carriers in 't = t (E). The classical law for the evolution of t is t = AE -s , in which s depends on the type of collision encountered. With eqn (21) which expresses (r) , following [smi 61], the calculation can give (t) ex A(kT)-s.
(35)
r,
In more precise terms, we can put t into the general formula 'teE) = 'to (k\ in which 'to is a parameter dependent on the nature of the interaction and the temperature of the lattice . When collisions do occur: •
on the lattice (collisions with phonons), when the temperature is sufficiently high, we have r = -1 /2, and 'to is proportional to T-' /2. We then have 't res = aE- 1/ 2T- 1, so that: ('t res) ex T- 3 / 2 as much as ILres ex T- 3/ 2 ;
(36)
on ionised impurities, then r = 3/2 and 'to ex T 3/ 2 , and 'tii = bE 3/ 2 , so that:
•
< r u> ex T 3/ 2 much as lL ii ex T 3/ 2 ; and on neutral impurities, then r ~ 0, 't ex TO , and
• l
-t
res
t
(37)
~ constant.
If we consider that neutral impurities are negligible, then here we also have ~ = + -L., which can also be equal to 1 = .L, + _1_ . Depending on the temperature [l
til
flre s
[l imp
regime :
-
1 ~ fl
~ ~
_1_
:ii
flre s
and IL ~ ILres ex T- 3/ 2 at higher temperatures (T 3/ 2 and IL ~ lLii ex
T 3/ 2
at lower temperatures (T 3/ 2
»
T- 3 / 2 ) ; and
« T- 3/ 2 ) .
416
Optoelectronics of molecules and polymers
b metallic conduction (cf. example given by [moo 93])
Metallic systems involve transport by electrons which are considered to be practically free and diffused by phonons and impurities, of which: -
-
the frequency of electron-phonon collisions (Wph), at a temperature higher than the Debye temperature, is proportional to the number of phonons (Nph), which is such that Nph ex T. Thus Wph = t~h ::::::: Nph ex T. With 0 ex 1:, the law of change of conductivity (Oph) as a function of temperature is Oph ex T- 1, and also Pph ex T; if the concentration of impurities (Nimp) remains independentof T, the frequency of collisions between carriers and impurities is Wimp = -t IImp ex Nimp, so that Pimp ex
_1_ = Timp
Po (constant).
If we assumethat the two collision mechanisms are independent fromone another, then we have as a total number of collisions W = Wph + Wimp, in whichthe average time betweencollisions (equallyelectron-phonon andelectron-impurity) is 1.r = .L + t ph _I_ . The upshot is that the resistivity ( p) is such that P ex 1. = .L t ,mp 't tph written, following Matthiesen's law:
P = Pph + Po = po (l
+ u'I').
Eqn (38) is useful at temperatures close to ambient.
+ _1_, and can be Tirnp (38)
A-5 General theory of conductivity in localised states: generalisation of the Kubo-Greenwood formula, thermally activated mobility, and localised and degenerate state bands
Even if the application of transport equations, usually obtained for ordered media in which it is a simple matter to define a reciprocal lattice-see Appendix A-4-is 'fanatically' classical, we shall now record how a general Kubo-Greenwood type expre ssion can be used to describe hopping transport mechanisms between localised states. We will indicate an expression for mobility and detail a new distribution function form which may be used in accordance with whether or not the Fermi level can be found in the band of localised degenerate or non-degenerate states.
I Expression for current intensity associated with hopping transport of a given charge placed on a specific energy level 1 Transcribing transport phenomena into equations We will consider that the transport here is of a given charge (q) which is initially placed on a certain energy level (E) (occupied with the probability f'(E) = fo which, very generally speaking, is the Fermi-Dirac function) . The tran sport is through hopping over a potential barrier of height U and situated between two sites A and B, each pair of sites for the moment having a given energy E. In the absence of an applied electric field, as in Figure l-a, the probabilities of occupation (fo) are identical for the two sites. Per unit time , transition probabilities from A to B and from B to A above the potential barrier U are also equivalent. We can therefore write PAB = Po exp (- ~) = PBA in which Po is the transition probability per second from A to B or from B to A with zero barrier and can be written as Po = ~ = ~ (as is the frequenc y of oscillation between two sites unaffected by barrier or external field). Once a barrier is set up, but still there is no external field, we have therefore
418
Optoelectronics of molecules and polymers d
(a)
d
(b)
Potential energy I
x
Figure 1. (a) A and B sites separated by a barrier over which hop carriers ; and (b) the modification of potential energies following application in Ox of an electric field (Ex).
or rather U
t
= toe IT .
(1)
In the presence of an applied electric field Ex which is directed with respect to Ox, as shown in Figure l-b, the potential energy W = qV for a charge q is reduced at Band increased at A (when q > 0). With Ex = -dV /dx , and supposing that Ex is uniform with respect to Ox, on taking the origin of the potentials in terms of O(V (0) 0) we have:
=
YeA) - YeO)
1 = 10 = 1 = ~O =
A
dV
o
Exdx
= Ex(O -
XA)
Exdx
= Ex(O -
XB)
A
2
B
V(B) - YeO)
o
dV
= Ex-d = YeA) . = -Ex-d = V(B).
B
2
For a charge q situated at A or B, the modification in energy due to the application of Ex is, respectively, W(A) = qE xd /2 or WeB) = -qExd/2 . It is noticeable that the energy increased by (qE xd/2) at A and decreased by the same quantity at B. Here we finally have an asymmetry with the A wells increased in height and the B wells pulled down . At A the barrier to overcome is reduced and becomes: V A = V - qE xd /2. At B the barrier is increased and can be written as VB = U + qE xd/2 . Consequently, in the presence of an electric field the transition probabilities, P AB and PBA, are no longer equivalent and become:
PAB PBA
= Po exp (
U - qExd/2) kT
= Po exp ( -
V
Exd
I +9 / 2 = -e kT t
+ qExd/2) = -e I _9 Erf 2 kT
t
1[
~ -
t
~
qExd/2] 1 + --kT
I [ qE xd/2] - I - --r kT
A-5 General theory of conductivity in localised states
419
2 Calculating the current intensity due to hopping mechanisms The current due to transport of a charge q between A and B, Ie, is the resultant of charge transport from A to B and from B to A, i.e. Ie = IA--+B + IB--+A ' It is the total charge moving per second in both these directions. If fo is the probability of site occupation at equilibrium and if 0 - fo) is, inversely, the probability of non-occupation, the quantity of charge moving from A to B can be written as IIA--+B I = qfoO - fO)PAB . Similarly, IIB->AI = qfoO - fO)PBA . As the currents lAB and IBA are in opposing directions, the resultant can be obtained:
which gives: Ie
= qfoO -
I
qExd j2 ]
[QEXf2
fo)~ e+
k
-
e----rr
xd /2) I sinh (qE = qfoO - fo)-2 -T kT
~
I [qExd] qfoO - 1'0)-2 -- , 2kT T
or rather:
I [qExd] le~foO-fo)T
kT
.
(2)
II Expression for current density and thermally activated mobility 1 Expression for current density relative to transport at a particular energy level The state density function for an energy level E being N (E) (number of states per unit volume of material) with in the volume V of a unit section is V = [S x d](S=I) = d, and the number of states with energy E is thus N (E)d . This is the number of individual charges (q) situated at sites with energy E (with T = T(E) for carriers leaving the sites). If we take a unit section between two sites A and B separated by the distance d, the current passing through this section thus becomes a current density with the value:
I(E)
2q = leN(E)d = -foO T(E)
xd /2) fo) sinh (qE -N(E)d kT
d] [qEx q ~ T(E) foO - fo) kT N(E)d, which yields :
d2 1 ICE) ~ q2Ex--foO - fo)N(E). 1:(E) kT
(3)
420
Optoelectronics of molecules and polymers
Figure 2. Schematisation of all possible hops through the section S = 1 giving rise to the currentJ(E).
2 Generalisation of the form of Kubo-Greenwood conductivity In order to assimilate all the possible hops-shown in Figure 2-through the section S, the length d must be placed in to terms of the mean free pathway (.C) the mean distance between two hops. In addition the current density, which involves all carriers from a volume V traversing the section S in both senses whatever their initial energy (E), can be written as:
J = q2E x
~
£2 I - - f o ( 1 - fo)N(E)dE E teE) kT
(4)
Again using the definition of conductivity (0') as that given by the relationship
J = crE x can be used to give a Kubo-Greenwood type equation : 0' = q
with
f
I1-(E)fo(1 - fo)N(E)dE,
£2 I !-L(E) = qt(E) kT ·
(5)
(6)
Comment With L = vxt(E), and with the help of eqn (4), we can go directly to: (J
=q
qv~t(E)
1 E
kT
fo(1 - fo)N(E)dE ,
a form of (J deduced from the Boltmann transport equation shown as eqn (14) in Appendix A-4. We can thus be content to use eqn (14), Appendix A-4, in which E = vxt(E) is introduced and from which we can directly obtain eqn (4). However, such a path tends to hide the physical reality of the problem which we have detailed in this Appendix .
3 Thermally activated mobility Following on from eqn (1), we have eqn (6) gives: 11-
t
= 'to exp
(&), and
on placing 11-0 =
= 11-0 exp ( - ~ )
This equation shows us that the mobility is thermally activated.
~~~ , (7)
A-5 General theory of conductivity in localised states 421 Comment
From eqn (6), we can write that
On posing
£2
D = -,
(8)
t
which has as dimensions a diffusion constant, we find Einstein's relation: kT q
D = -~.
(9)
While the study of transport with respect to the direction of the electric field does not a priori require the introduction of the coefficient 1/6 , we can have the isotropic diffusion . I (0) with P = - . r
III Approximations for localised and degenerate states Here the calculationsfor conductivity can be performedusing the Kubo-Greenwood relationship i.e. (J = q f ~(E)fo( I - fo)N(E)dE, but require,in general, thefollowing approximations: -
as thestatesare neighbours at the levelE = Ep, we assumethatN(E) ~ constant = N(Ep); and ~ = ~o exp (- k~) = constant with respect to E, as in ~ (E) = ~ (Ep).
The calculation for (J requires therefore the evaluation of (J
= q
~o exp ( - ~) N(Ep)
f
fo(l - fo)dE.
We must therefore go on to evaluate f foO - fo)dE. This can be done using eqn (2) of AppendixA-4, so foO - fo) = -kTt . Figure 3-a represents the Fermi function and Figure 3-b the function - t . At not too high a value ofT, (T ~ T, = 300 K), the above schematicrepresentation shows that t behavessimilarly to a delta function, so that
Thus:
f f
kT
(~~) dE ~ kT.
foO - fo)dE ~ kT.
When a high number of defaults result in deep localised states within the gap, we find that (Be - Ep) » kT, and carriers cannot be thermally excited into
422
Optoelectronics of molecules and polymers (a)
dfO dE
(b)
/~...TTo=OK
•.
. . . . . I \ . . .( '"/ •.•••••
.' I
1
r,:» T 1
X/ ••••••
::
.
E
Figure 3. Representations of: (a) the Fermi function; and (b) the function ~ .
the conduction band. These carriers remain localised around EF in a degenerate band of states. The transport process in the neighbourhood of EF is realised by bringing into playa density of charge carriers given by n = N(E)foO - fo)dE ~ N(EF) foO - fo)dE ~ kTN(EF)· The conductivity is thus in the form o = q kTN(EF)f.LO exp (and is thermally activated by the form of the mobility.
f
f
Ji.)
A-6
Expressions for thermoelectric power in solids: conducting polymers
I Definition and reasons for use 1 Definition Under the effect of a temperature gradient, there is a diffusion of carriers from hot to cold points which is associated either with a concentration gradient as in the case of semiconductors, or a velocity gradient of carriers in the case of metals . The result is an excess charge and, in effect, the birth of an internal electric field (E). The resulting ~
~
-----+
current is the sum of two parts : j = crE + M gradT
At equilibrium the current is zero and the internal field is such that: ~ ~ gradY VA - VB E = S gradT, so S = - - - = - - - gradT TA - TB
!1V !1T
in which , by definition, S is the Seebeck coefficient.
2 Reasons for use The parameter, called thermoelectric power (TEP) is: •
•
an intrinsic property of a material and is independent of the geometrical dimensions and insensitive to faults such as cracks, in contrast to other properties such as conductivity; and essential to distinguish metals from insulators and understand which carrier is in the majority in a particular material.
424 Optoelectronics of molecules and polymers
II TEP of metals (EF within a band of delocalised states) A rigorous calculation must be performed within the context of the Boltzmann transport equation:
For a metal close to the Fermi level, we have (d In o I dE) < 0 and therefore Sm > O.
N(E)
On developing the calculation with o(E) ex aE' and [dlncr(E)/dElEF ~ liEF) we have the following equation:
Sm
~
k Jt2 kT
-- q 3 EF
~
several u V/K .
°
Thus Sm has a low positive value and Sm = f'(T) is linear with Sm -+ with temperature. Qualitatively speaking, we can say that with a good metal the thermal gradient does not practically 'destroy' the equipotential at its surface and that ~ V ~ 0, so S is very small .
III TEP of semiconductors (SC) (EF in the gap)
A-6 Expressions for thermoelectric power in solids: conductingpolymers 425
1 Preliminary remark In a metal the diffusion of hot electrons of charge -q, takes place above EF and therefore the effective negative mass is such that the associated force is directly opposite to the diffusion velocity: :::} VA < and VA - VB < 0, which gives Sm > 0, as we have already seen . For SCs , the carriers (-q) have m" > 0, so, only in p-type SCs , we have carriers with +q and m" > 0. In order to determine the force applied on the carriers, (+q or -q), we can use f = m*y with y IIv and m" > or <0).
°
°
A
2 An ideal n-type semiconductor Locally around A, the concentration of carries increases with the effect of t::. T (n ex T 3/ 2 exp(- [Ec - EF]/kT) . The result is that electrons diffuse from A towards B (m: > fel Iv) where a charge < 0 appears. And leaves a charge > 0 at A. We can thus write that VA - VB > and TA - TB > 0, so that SN < 0 .
°:: }
°
r. More quantitatively, without going through the rigorous treatment of the transport equation) we have S = (Kelvin's 1st relationship), where IT is Pelletier's coefficient. For electrons, with the energy transported per unit charge and by taking the potential origin as EF, and then with
¥
Energy = Ppotential + Ekinetic, Epotential = Ec - EF, Ekinetic
~
Ec - EF +2kT 2kT : IT = - - - - - -
-q
C
Ec
E"
---f 2kT
426
Optoelectronics of molecules and polymers
Finally: with here B = 2 Thus SN < 0 and typically goes in value from a hundred or so I-L VK- 1 to more than several mV K- 1 .
3 An ideal n-type semiconductor The diffusion of holes (+q , m~ > 0) with ftl [v results in charging B positively (while leaving a negative charge at A). So we have VA - VB < 0 and TA - TB > 0, and that Sp > O. Thus :
Sp = -k [EF - s, +B ] , q kT
here with B = 2
A f
T+~T
4 Comment on amorphous semi-conductors for which Ec - EF = b.E - aT. For a n-type semiconductor, for example, SN = -
~q [b.E - ~ + B] kT k
while S = f(l/T) and In a = f(l /T) exhibitthe same slope . The ordinate at the origin for S = f(l /T) yields a .
5 A non-ideal amorphous semiconductor with EF below its states in the band tails Here the carriers have a thermally activated mobility in the band tails and I-L = I-LO exp( - U I kT ). The form of the tail band is such that N (E) =
N (Ed (E - EA)S (Ec - EA)S
and calculating S within Boltzmann restrictions gives S=
_~ q
kT
[EA - EF kT
(a ~ aoC s ( Ec _ EA
+ ~] Cs+1
)S (EA - EF + exp kT
U)
A-6 Expressions for thermoelectric powerin solids: conducting polymers
427
as discussed in Chapter V, Section IV-I) .
Conclusion The slope of In (J = f (1 IT) is larger than S = f (1 IT ) by an amount U, and is characteristic of this transport mechanism within tail band localised states (in the absence of localised states in the band tails, the two slopes are identical.
IV TEP under a polaronic regime We will distinguish between high and intermediate temperatures in a manner similar to that used for conductivity.
1 High temperature regime Here, S can also be deduced using Kelvin's l st relationship, S = rI/T in which Pelletier's coefficient (energy transported per unit charge) is such that we can suppose that the polaron does not transport the vibrational energy IT = ~ (Eo is the energy which characterises the thermal generation of carriers and Eo = Ep - EF). From which we can deduce that in the high temperature regime, S = -
~
(f¥).
2 Intermediate temperature regime The regime implicates a VRH transport mechanism and, as we shall see in the following Section, S follows a law of the form SIT = f(T- 1/ 4 ) .
3 Other regimes It has been found that for amorphous semiconductors, S ~ Cte with respect to T. Nagels proposed that with the concentration of polaron s being constant with T, S follows Heikes law which is of the form S ~ -(k/q)Ln([N - nj /n), in which N is the number of sites and n is the number of carriers .
V The TEP for a high density of localised states around EF 1 Initial hypothesis If EF were to 'dive' into a band with a high density of (localised) states, it has been supposed that the expression used for a metallic system for the TEP would still be
428
Optoelectronics of molecules and polymers
valid by Cutler and Mott. In reality, however, experimental results have shown that S i= 0 as T ~ 0 in complete discord with the hypothesis.
~
BC
1----------
BV
...
In fact Nagels has shown [Nag 85] that in the low temperature domain we can write: S= _
Jt2
~KT {d(lner(E)}
3 q
dE
E=EF
and that c(E) is expressed as a function of N (E) for which we assume that close to EF there is a linear variation such that N(E) = N(Ep)[1 + y(E - Ep)] with yW « 1, in which W is the height of the hop .
2 The result in VRH Here we follow the work of Nagels in J. Non Cryst Sol. (1983) and consider the VRH condition with respect to the optimisation of both the hopping distance and the hopping height (W(E», the calculation of S, with y = (1/N(EF)[dN(E)/dE]E=EF, gives:
Comment The advantage of the above calculation with respect to other possible routes is that it brings in the factor y which takes into account variations in N(E) near to EF and does this independently of the origin of the states in the gap disorder, polarons etc.).
A-6 Expressions for thermoelectric power in solids: conducting polymers 429
VI General representation In (J
E
(E)
VRH .---
I
;
Ec
i
EA - E.,
!
:.1-
_
q
Iff
Iff
VII Real behaviour 1 Generallaws a Different levels of conduction participate in parallel The law is derived from the general equation itself generated from the Boltzmann formalisation, and is such that
As an example, we can site the conduction by both electrons and holes in S = GeS e + GhSh , Ge + Gh and that in an intrinsic semiconductor we have
b Differing domains in series Kaiser proposed [Kai 89] that during a drop in temperature, is remain proportional to the thermal resistance (Wj) of each domain, sothatfromS = -!1Vj!1T = -(!1Vl +
430
Optoelectronics of molecules and polymers
fj, V2) 1 fj, T = (fj, Ti l fj, T)SI + (fj, T21 fj, T)S2 we can deduce that S (W2/W)S2, with W being the total resistance.
= (WI /W)SI +
2 Behaviour as a function of dopinglevels
a Highlydoped conducting polymers In addition to the metallic component in S, it has been observed that at low temperatures there is a distortion of which Kaiser brought into account by using a non-linear component A. *(T)T associated with effects on the carriers due to phonons. The resulting equation is therefore:
b Moderately dopedconducting polymers Here there are two ways of looking at the scenario:
•
•
EF is more or less outside of the extended states and the system tends towards a semiconductor character => SIT ex -y(ToIT) X(see also Section y) or the system is an ideal semiconductor in which case exhibits a slope [Ec - EF] /q with l iT) ; and that we have a heterogeneous structure (Kaiser, Phys Rev 1989), with conducting fibres separated by barriers and we have S = (W t/W)SI + (W2/W)S2 = XT + CT 1/ 2 . The first term in this equation characterises the (metallic) transport along the fibres while the second term, for inter-barrier hops, follows a VRH type law with respect to T I / 2 de type proposed by Mott. If the barriers are thin and conduct heat better than electricity, we can simplify things by assuming WI » W2 and that S ~ XT (see also Section a).
c Poorly doped conducting polymers (EF is placed within a quite large gap that has few states and the material is close in character to an insulator). Whether looking at polaronic states or states tied to locali sed defaults, at low and intermediate temperatures, in principle they both follow a VRH law in the form SIT ex f[T- 1/ 4 ] . Indeed, under certain conditions, such as in the impurity band, Heikes law can be envisaged so that S ~ -(k /q) In([N - nj /n) is reasonably constant or decreases only slightly with T.
A-6 Expressions for thermoelectric power in solids: conducting polymers
431
3 Representational graph
lsi Mode rate to weak dopin
Weak doping:
(SC'mlronducdng statr "Ith ffl' loaal l....t . ta les) Is I • Iklq)( (MAT) + HI
s .. etc with T
II rik". la",'
Weak doping: (ma o) IQClIIi....t
l~l <'l )
Is I rr = 1 f(T .IJ~) trong dopi ng: S > 0 and S =XT (' meta l')
_ .J.*: distorsi o ".
T(K)
4 An example result An useful example is that with reversible doping-performed with ion implantation at 30 keVin poly(para-phenylene)-followed with respect to the changing positive and negative value of S [Mol 98]. In the Figure below, the curve (a) shows the variations of a sample initially made p-type using iodine and then doped to n-type by an increasing flux of n-type alkaline ions. Curve (b) shows the effects due to a sample undergoing initial n-type doping with alkaline ions and then a subsequent implantation with an increa sing flux of halogen ions.
60 Initial iodine implan tatio n
~
40
;;. :::l.
.
~ ~
D: Flux (ions cm"2)
20
OJ
~ 0
e,
..E'" 0
:S ~
=
(D 5 X IOU). followed bv C. impla nta tio n
0
- 20
- 40
- 60
A-7
Stages leading to emission and injection laws at interfaces
I Thermoelectric emission and the Dushman - Richardson law With W s » kT , we have E - EF » kT and the Ferm i function tend s towards the Boltzmann function: f eE)
~ exp( -[E -
EFl/kT) = exp ([EF _
h;~2 ] / kT) .
So that an electron is emitted in Oz-simpl y through therm al agi tation- and without takin g into acco unt a reflection coeffici ent, the equ ation [(E)selon 01. - EF1:::: Ws must be true , as schematised in Figure I . Given that the energy is uniquely kinetic than the emission co ndition is thus [El in 01. =
h2k1.2
2m :::: EF + Ws =
h2k 2
2~O .
(I )
We will define the numb er of electrons as dn in the reci procal space volume d 3k . Th e latter is divided into elementary cells so that ~ kx ~ ky ~k1. = ~k 3 and
~k3 = 8~3 . On reasonin g that V = I (dn will be a density) and the possibility of placin g two electrons per ele mentary cell (due to electron spin), we have: 3k
dn
= 2 x [number of cells in d 3kl x f(E [k]) = 2-d
8n 3
f'(E) .
Th e elementary current density (dl 1. ) emitted in the direction Oz and effective for dn electrons is therefore h 2 k1. d 3k hk 1. dJ 1. = d p V1. = e dn V1. = e dn --;- = e 4n 3 exp (EF/ k'T) exp( - E/kT) ~. The emi tte~ current density ca n be obtained by adding over all electrons which have a vector k with a component k1. which complies with the already establi shed condition eqn (I): h2 k 2 h2 k 2 __ 1. > E +W = ~ 2m - F s 2m ' whatever the other compo nents k, and kyo
434
Optoelectronicsof moleculesand polymers k,
w, EF Conduction band Ec
--I:..::..I:..::..:..::..:..::..:..::I-----'--....I.--1~-___jf+--_+----=--...>I.<:'--t_-_+f__.
Metal
Figure 1. Schematisation of the thermoelectric emission condition.
Therefore:
With kzo = 2m(E~tWs), on calculating by way of the well known results for integrals
1
+ 00
-00
e- ax2 dx = ~ and a
+ 00
1 zo
I 2 ze- a z dz = _e- a zo , 2a
we arrive at the desired equation:
(2) Exactly speaking, a reflection coefficient R should be introduced to take into account any possible reflection during emission. An example of this calculation can be given with tung sten (Ws = 4 .5 eV). 1.2 x 106 A m- 2 K and ~ ~ 19 at T 2700 K, the calculation gives With A J = 2.2Acm- 2 .
=
=
II Schottky injection (field effect emissions) Here we have an increase in the thermoelectronic emission due to the lowering of the barrier (Ws in thermoelectronic emission) due to the electric field effect applied at the metal (electrode) interface.
A-7 Stages leading to emission and injection laws at interfaces
435
1 The potential barrier at the atomic scale On the atomic scale at a metal-vacuum or dielectric interface , the potential barrier observed by an electron extracted from the metal is not an abrupt step (see Figure 2-a) . In effect, an electron situated at Z > 0 in an insulator is not completely free and to distance itself from the metal is must overcome the attractive force exerted by the latter material due to the image charge (+q) which the electron induces in the metallic electrode (see Figure 2-b). For an electron (-q) on the z abscissa, its image (hole +q) is at a distance 2z. The force which is therefore exerted on the electron, which is in an insulator that exhibits absolute permittivity s, is thus
_
q2
F= -
4TI£(2z)2
q2
~
= - - -2 = -grad We
16mz
'
in which We is the electro static energy. In l -dimension, We(z) - We(oo) = We(z) = -
z lz l Fdz =
00
00
q2 q2 = --16TI£z 16TI£z
--2
(with the origin s of energy at infinity).
Comment The above representation is only acceptable when the distance z is large with respect to the interatomic distances . When z ~ 0, We(x) is brought towards the potential energy level at the bottom of the conduction band (Ec) . When z = 0, we join the energy of the electrons to Ec . 2 Emission conditions: Schottky emission law and the decrease in the potential barrier by field effect a Without an applied field Here the condition (E)in Oz ::: EF + Ws must be fulfilled (in the Oz axis) using the metal side as the origin of potentials in the lowest conduction band (in Ec ) . With the Potential energy
o v W, W(z)
=. 167lEZ
r
+q Metal
z
q2
vacuum
'4
~.-q
(elef tron) Zz
.'
Figure 2. Graphical representation s of: (a) an electrode potential as seen by an electron at the atomic scale; and (b) the charge image (+q) of an electron.
436
Optoelectronics of molecules and polymers
energy of electrons exiting being solely kinetic energy, we should be able to apply condition (1) which can also be written as tmv~ ~ EF + W s.
b In the presence of an electric field The field is applied so that the metal has a negative potential (cathode) and the part external to the metal is positive . We have -
F
----+ = -grad We = -qEa ,
and We(x)
=-
10t
qEadz
= -qEaz.
Thus, the total potential energy of an electron situated at a distance z from the surface becomes:
q2 WTotal= - qEaz - - - .
16€z
The resulting curve presents a maximum in Zm , which is such that
(
= 0,
OWTotal )
OZ
and Zm
=(
6q
) 1/2
1 Jt€Ea
Z=Zm
The result is that
The work function is reduced by an amount b. W s = IWTotal(zm)l, a value not more than
W~ =
Ws
-
qlfi (see Figure 3).
The emission condition (I) now becomes the condition (1/): tmv~ ~ EF + W~.
Potentialenergy
o
--
w,
--- ---- --------
Dielectric or vacuum Metal
q2
WTotal = -qEaz - -16
nez
Figure 3. Energy diagram describing effects due to application of an electric field.
A-7 Stages leading to emission and injection laws at interfaces
437
Log JSch Schottky straight line //~
Log J//
.... ~
/ Effect due to space charge
Figure 4. Representation of Log JSch = f
(JE;;").
Eqn (2) for current density is this still usable, as long as W s is replaced by W~. in teh presence of an electric field the emitted current density thus becomes 2
J = JSch = AT exp
-
( [
rqE;])
ws - kTqy' 4rr'E
.
(3)
For a give value of T, Log JSch = f(JE;;") is a straight line. Nevertheless, in practical terms, we can observe at low values of E a deviation from the linear law and this is due to the appearance of space charge close to the emitting surface (see Figure 4) .
b Comment using numerical example With E, = 104 V m -I , we have (Figure 3) Zm ~ 0.2 IJ-m, while with Ea = 1019 V m -I, we find Zm ~ 0.7 nm. The height of the potential barrier is reduced in the first case by ~ Ws = 4 x 10-3 eV, and by ~ Ws = 1.2 eV in the second. In a strong field, ~ W S ~ W S and the height of the barrier to overcome is extremely low, so that breakdowns can occur under high fields (Ws[Cs] = 1.8 eV; Ws[Th] = 3.35 eV and Ws[W] = 4.5 eV).
III Injection through tunnelling effect and the
Fowler-Nordheim equation 1 The problem As the applied electric field increases, the height of the barrier observed by electrons close to the Fermi level actually decreases. This in tum greatly facilitates the passage of electrons over the barrier (field emission due to a Schottky effect). In fact, another mechanism appears once the field is increased. As shown in the qualitative example just above, as E, increases Zm decreases; also we can perceive a qualitative decrease in the barrier. If the barrier decreases sufficiently then the probability of electron presence, initially close to that of the barrier (in terms of Z is equal to 0), turns to being non-zero at the other side of the barrier. This is due to the wave like character
438
Optoelectronics of molecules and polymers
of electrons , which is accounted for in the probability of presence at the point z being written as P(z) = 1'\jJ(z) 12. The barrier transparency can be calculated for simple cases . Before going in to the calculations, we can remark that if E, increases , then the effect due to the force image-which is predominant in a weak field and in Schottky emissions (close to z = zm)-diminishes when we are at a sufficiently high value of z. This can be a point, for example, in the region of z ~ ZF (defined in Figure 5 in which ZF corresponds to the point at which E = EF). On the side of the insulator, the potential energy there is simply approximated to using the field effect of the electric field so W(z) = -q E, ZF, in which ZF is the size L (such that ZF = L) of the barrier seen by electrons situated at E = EF. Thus q E, L = Ws, that is Ws L=-
(4)
qEa
In effect, the higher the value of Ea , the more narrow the barrier. In the case of tungsten, we can use Ws = 4.5 eV and E, = 4.5 x 109 V m- I to calculate that L = 1 nm. At high enough field strengths, the barrier becomes sufficiently narrow to present a non-negligible transparency to electrons free in the metallic electrode.
2 Form of the transparency (T) of a triangular barrier The transparency
cn of a barrier is usually defined by: Flux of transmitted particles Flux of incident particles '
T=----------''----
in which the flux represents the number of particles which traverse an unit surface area per unit time. The flux can this be represented by the product of the probability of
o
__ ___ ___ ____L zr =L
I I I I I I I I I
Ws
Function (E) for T ,*OK forT = OK .... .................. ......... ...
--. 1
"""1---
Line of the equation W=-qE.z
.......::::w
(E)
Figure 5. Diagram of potential energies for tunnel effect emissions.
A-7 Stages leading to emission and injection laws at interfaces
439
presenceper volume with a unit section and a length v (if v denotes particle velocity) (see Figure 6). It is possible to write eqn (5) for a barrier of length L by assumingthat the initial velocityof free electronsin the metal (Vi) and their velocityafter traversing the barrier (vd are such that Vi ::::::0 VI: 2 T _ vtltlrtransmisl - viltlrincidentl 2
::::::0
2 2 Itlrtl _ ItIr(L)1 Itlril 2 - ItIr (0) 12 .
(5)
In this problem, it is reasonable to think that the most important part of the injected current, following the applicationof a field, will come from electrons which have an energy close to the Fermi level as the distribution function N(E) has as maximum E ::::::0 EF . Thus the expressionfor T of the barrier is given by eqn (5) in which L is the size of the barrier observed by electrons for E = EF (Figure 5). In order to calculate the size of the barrier more precisely, we shall have to look at the origin of the energy at the EF level by treating a classical rectangular barrier with quantum mechanics (see Figure 7). Weshalllook at electronswith an energyE,just aboveEF anddenotetheir velocity v when z < 0 and v' when the electrons are at z > o. Generally, the conservation of energy for an electron placed initially at the level E, (neighbour to EF) and then at A after having traversed the barrier can be written, using the notations detailed in Figure 7, as: E, =
2I m v2 = 2I m v12 + U(z)
from which can be deduced m2v'2 = p'2 = 2m(Ei - U(z)), so that with k'2 = ~~ we have k'2 = 2m(\~U(z)) . For E, < U(z), k' (z) is imaginaryand I
.
k (z) = J
[2m(U(Z)-Ei)] 1/2 n}
The wavefunction, in the form ei kz for free electrons and with a real k, takes on the form tIr(z) = eiftk'(z)dz. .
T can be wntten therefore as T ex
:..
ItIr(L) 12 -2 L ( 2m ) 1/2 [U(z)-Eil l / 2d z 2 = e fo fiI , ItIr(O) I
~:
z = (v ~tht=l=
V
Figure 6. Geometric parameters required to define flux.
440
Optoelectronics of molecules and polymers
Figure 7. Representation of a triangular barrier.
and definitively
T
= feE, W s) exp
2m] [ ! -2!if
Jo[L [U(z) -
1/2
Ed
l/ 2
dz
I
(6)
.
3 The Fowler-Nordheim equation
In the relationship (6) for T, the term to integrate, [U(z) - Ed , is such that: [U(z) Ed
= Ws - qEaz - Ei Thus
l
L
o
= u(z), so that u'(z) = -qE.
[U(z) - Ed l/2 dx =
lL
[u( z)]1/2 dz = - I
l
L
[u(z)]1 /2du(z)
qE 0
0
I2 ( u(z) = -qE 3
3/2)L , 0
and on taking into account eqn (4):
1 L
1 2
[U(z) - Ed I dx
2![
= - qEI 3" 2 I
W s - qE
~ __ W~/2 , as
3 qE
Ws - Ej ]3 a qEa
/2
3 2
- [Ws-Ed I
I
E, «Ws
(and notably at T = 0 K). Finally:
T=
2m) 3"2qEI W~/2 ] .
rrs. Ws) exp [- 2 ( li 2
1/2
(7)
a
As L = ~:' we can see that (T ~ 0 K) the transmission coefficient is an exponential function of the size of the barrier. Only electrons very close to EF can leave with a non-negligible probability.
A-7 Stages leading to emission and injection laws at interfaces
441
When T =1= 0, electrons situatedjust above EF are privileged as even though they are few in number the actual barrier they have to cross is thinner. The Fowler-Nordheim calculation performed at OK does nevertheless take into accountall electrons.In using the fact that the currentdensitycontributionfrom levels situated in the interval [Ej, Ej + dEj] is in the form dJ = q N(Ej)T(Ej)dEj, the sum over all the E, states results in a current density of the form: J=
q3E~ exp[_~(2m)1/2W~/2] .
8JthWs
3!i2
qEa
(Note that N(Ei) dEi is the number of electrons hitting the unit surface area per unit time with an energy between E, and E, + dEj). Numericallyspeaking we can use this equation as in: 3 2) a exp ( -6.83 x 109 _ Ws /_ J(Am- 2) = 1.54 x 1O-IO_E2 Ws Ea
.
The above relation shows that the current density emitted for this process is negligibleat E, < 108 V m- I , and that it increases rapidly at higher field strengths. = f(J) arethe linesdrawnfor thesetypesofemissions Ln( ~2) = f( ~) or Ln( a and linear behaviour over a decade of l/V can permit determination of W;
b)
Comment The obtainedequationsrelate to emissions into vacuum (barrier Ws seen by electronscomingfrom the metal).When an emissionis into an insulatorthe barrier to overcomefor the electronscomingfrom the metal isjust WB = (Ws - 'tJ, where X. is the electronaffinity of the insulatoror semiconductor. WB can be substitutedfor Ws is the equations (see the Fowler-Nordheim equation is Section IlIA of ChapterVI).
A-8
Energy levels and permitted transitions (and selection rules) in isolated atoms
This Appendix gives a brief, but ultimately essential description of the construction of energy levels in an atom which appear under the effects of succe ssive perturbations, going from the most to the least intense .
I Spherical atoms with an external electron Typically the titled scenario resembles that of hydrogen atom s, but it can also be applied as a first approximation to the more general problem of describing an atom with more than one electron (through the potential, observed by an electron, being approximated as a symmetrical sphere).
1 Energy levels and electron configuration [Cag 71] Given the symmetry of the system under study, the energy levels can be obtained by assuming that each electron moves, to a first approximation, within a potential sphere which originates from the nucleus potential and the spherical potential which globall y repre sents the effects due to all other electrons. The states of the electron orbital s (without therefore taking into account spin) are written using an electron orbital wavefunction (1/Jn,l.m/ = Rn,18t,m\
+
-1,+1'
444
Optoelectronics of molecules and polymers
In addition, the invariability of the Hamiltonian of the system during a rotation shows that the energy levels (E) of a spherical system depends only on the two quantum numbers nand 1so that E = E(n , 1). Thi s can mean that the system is highly degenerate and at a given energy level E(n, 1), we can associate [21 + 1][2s + 1] electronic state s repre sented through electronic wavefunctions ('!J(n, I, mi, m.) 0 , using Dirac notation, In, 1, mj , ms from orbital and spin wavefunctions. In order to know the total energy of an atom , we need to sum over all the energies relating to each of its electrons. Thi s requires an understanding of the spread of electrons with respect to layers and sub-layers, as defined by the quantum number nand 1, respectively. In other word s, the atomic configuration of the atom must be known. To denote this, each layer is symbolised by a number equal to the principal quantum number (n) following by a letter which repre sents the value of the quantum number I (for 1 = 0, 1,2,3 ... the letters are, respectively, s, p, d, f ...). When several electrons are in the same sub-layer, we just write the symbol denoting the sub-layer once , and then add an indice indicating the number of electrons in that sub-layer. As an example, we can write the configuration of sodium, which has II electrons in all, as 1s2 2s 2 2 p6 3s. The filling up of layers with electrons occurs in a specific order defined by Klechkowski's rule, which states that it follows the increasing order (n + 1). For a value given which is the same as (n + 1), then it is the value which corresponds to the lowest value of n which is filled first, as shown in Figure 1.
»
2 Selection rules In this Section we finally have to con sider the conservation of kinetic momentum and how, for a lone atom with one electron, there is a radiative transition . this occurs when the variations in quantum numbers of the energy levels involved concord with : • •
~n = any integer (as the principal quantum number is not tied to kinetic moment and governs only the energy level) ; and ~l = 1 (as in, for example, the transition from the p-state [l = 1] to the s-state [I = 0] is radiative, as for the transition d -+ p, however, the transition d -+ s is forbidden and is therefore impos sible with photon emission.
II n
I
2
3
4
5
S
S
Ws
1 !-4 0 I 2
S-
I S
rI
"p " :tV If; IitP ;y
cV
d
Figure 1. Filling up layers following Klechkowski's rule.
A-8 Energy levels and permitted transitions (and selection rules) in isolated atoms 445
II An atom with more than one peripheral electron In addition the electron configuration (y) , which uses only the n and I quantum numbers to repre sent energy levels and only includes a global, symmetrical, spherical potential repre sentation of electro n interaction s, we need to take into account success ively: •
•
the exact electrostatic interactions between electr ons which introduce into the Hamiltonian of the system a perturbation operat or Hee, which raises the degeneration of the system; and weaker perturbation terms which progressively raise the remaining degeneration in the energy levels. The nature of the perturbation terms which must be succe ssively introduced depend s on the type of atom under study-whether it be heavy or light , with the limit generall y around the mercury atom (Z = 80) , along with its environment, for example whether or not it has been inserted into a matrix. The latter effect has been discussed with respect to atoms with incomplete inner layers in Chapter VII, Section II.
1 First effect produced from the perturbation H ee due to exact electronic interactions The Hamiltoni an of the system is only invariant when there is a simultaneous rotation of all electrons. Thi s can be assoc iated with an orbit al resultin g kinetic momentum operator and a spin resultin g kinetic momentum operator. We can show, relatively simply [Cag 71, Mol 81], that the energy levels from an electron configuration (y), under the influence of a perturbation Hee , correspond to energy levels (E) in the form E = E(y, L , S). For an atom with two periph eral elect rons, respectively characterised by quantum numbers I I and s I for one, and band S2 for the other, L and S are such that they vary by whole values in the Clebsch-Gordan series, so that L = II - lz II + 12 and S = S ] - S2 S l + S2. The electron states are, for their part, written using a wavefunction in the form Iy, L, S, ML, Ms ), in which ML = -L, (-L + I), . . . . + L and Ms = -S , (-S + I), .. . , +S, so that the energy levels are degenerated (2L + I) (2S + 1) time s. The fundamental state is thus determined from Hund 's rule which indicates that the lowest energy terms that for which: •
•
S is the maximum (because from Pauli 's principle, taking on the maximum spin implicate s a distinction between states by their orbital states which must thus b different and minimi ses electrostatic interactions by distancing electrons); and L is a maximum after taking into account the above condition.
The spectral terms, which relate to the different states, are thus denot ed by an approxi mation n2S + IT , where T is one of the letter s S, P, 0 or F for which L takes on respectively to signify one of the values 0, 1, 2, 3 . . .. If we take Cr+++ as an example, it has the configuration 3d 3 , and we find:
446
Optoelectronics of molecules and polymers
!
Smax = 3 x = ~ As I = 2 (sub-layer d), we have mr = -2, -I , 0, I , 2 and (L mt)max = (Mdmax = 2 + I + 0 = 3, wherein LMax = 3. By consequence, the fundamental state of Cr+++ is 34F (denoted simply as 4F).
-
2 Perturbation involving the coupling energy between different magnetic moments exactly tied to kinetic moments Two different cases can be distinguished: a when the spin orbit interaction energy is weak (typically for atoms with masses below that of mercury) In this case we use Russel-Saunders coupling, which is generally considered to not be significant until we have coupled it up with, on one side, all the orbital kinetic moments and, on the other, the total spin kinetic moment s. It is only after this that ~he tw~ kinetic moment s interact through the intermedi ate of spin orbit coupling. L and S represent the resultant of this total couplin g. The pert~r~ation Hamiltoni an due to the spin-orbit coupling is in the form Hs.o. = )"(L, S)L.S in which )"(L, S) is positive in the first half of the layer. With 1 = L + S ....L - S, there is a rise on the degeneration of the energy levels which is given by the proper values of the perturbation Hamiltoni an Hs.o.:
~E =
S 2 )..(L'2 )1i [1(1 + I) - L(L + I) - S(S + I)].
The spectral terms are thus denoted n 2s+ ]TJ, in which T corresponds, as above indicated, to the letters S, P, D and F which as values of L are, respectively, 0, I , 2, 3 . ... The upper left indice gives the number of possible orientations of the resulting spin, and is called the multiplicity of the term (doublet, triplet and so on), however, one needs to be prudent in using this notation. If S < L, then 1 takes on 2S + I and the number of values for 1 is given by the upper left indice, however, if S > L, then 1 cannot be negative and can only take 2L + I values and therefore there are only 2L + I permitted levels. In the case of Russel-Saunders coupling (also termed L - S coupling), the schematic representation of increment s in degeneration of energy levels under the influence of increasingly small perturbations are shown in Figure 3. For example , from the level L'S' degener ated [2L' + 1][2S' + I] times (resulting from exact electron interaction s, also called electron correlations) the spin orbit coupling is partially raises the degeneration so that I ' takes on [2L' + I] or [2S' + I] values (denoted as the values 1; , 1~ , 1~ in Figure 2). b Heavy atoms-jj coupling When the spin and orbital kinetic moments of each electron are coupled in the first step (with the resultant kinetic moment ji for the ith electron again obtained from
A-8 Energy levels and permitted transitions (and selection rules) in isolated atoms
447
L'" S"' L" S II L' S' J~ L'S' J~
Y(n,l) L'S'
L' S' J~
configuration LS
Spherical potential
Electronic correlations (Hee)
Spin orbit interaction
Figure 2. Levels of degeneration in L - S coupling .
terms of the Clebsch-Gordan series) , the resultant kinetic moments of each electron are then coupled between each other (jj coupling) to yield a global moment J. For an atom with 2 electrons with kinetic moments jj and j2, J takes on the values J =
Ijl - j21 ,··· .i. + j2. 3 Selection rules There are two final cases to consider:
a Russel-Saunders coupling for light atoms with several electrons The emission or absorption of light, which requires a variation by one unit of the kinetic moment, can happen when (selection rules) : •
LlS = 0 and the optical wave does not affect the internal movement of the electrons;
• •
LlL = ± I, 0 with Lli = ± I (l is the kinetic moment of an electron which undergoes the transition, while L is the kinetic moment of the atom ; LlJ = ± I , 0, however, the transition J = ~ is forbidden.
° °
b jj-Coupling for heavy atoms with several electrons The Russel-Saunders coupling selection rules are not applicable to heavy atoms with several electrons as the Sand L quantum numbers no longer have any physical significance, as the effective jj coupling suppresses the coupling of orbital moments to give L, along with the coupling of spin kinetic moments which give S. In this eventuality, transitions between singlet and triplet states S = 0 ~ S = I, where LlS i= 0, become possible (jj coupling for heavy atoms) . However, the condition LlJ = ±1 , 0 with the forbidden transition J = 0 ~ 0, remains [page 372, Cag 71].
A-9
Etching polymers with ion beams: characteristics and results
I Level of pulverisation (Y) 1 Definition y = (Mean number of ato~s .ej ect~d from target) number of incident IOns for a given ~t
In effect Y = f (E, J, e, M I, M2), in which M2, E, J and e are, respectivel y, the mass of the target atom , the energy of the incident ions (MI), the incident ionic current density and the angle between the incident ion beam and the normal to the target surface. With : • •
the energy transmitted to B during a sequence of colli sions (TB); the energy of the surface bond (Us) reason ably estimated to be equal to the sublimation of the target, so around 5 to 10eV,
the condition for ejecting an atom from the target is that TB ~ Us. There are two possibl e sequen ces: For the threshold energy, either ESI for sequence I or E SII for sequence II, and with the energ y of displacement as Ed, and 2M]M2 Y= (M] +M2)2 '
450
Optoelectronics of molecules and polymers
y
- equence I efficient for e =0 (normal incidence )
- Sequence II efficient for 11 ~ M2.
ESt
/
/rl T)'p~
Es" o T.
I collisio n sequence
Typ« /I collision
~qu. na
it is possible to write that
and
2 ESII = - (2Us y
+ Ed)
2 The result Yphysicat = f'(E): 3 zones Y (pulverised atom s/incident ions )
(IIy -(I)
() E,
I: below threshold (T B ::; Us ); II: E ~ E s and threshold energy fixed by sequence type I or II (TB ::: Us ); and III: when E > Es, rapid increase in Y, then a saturation plateau (reached rapidly if mass M I and M2 are grea tly different).
A-9 Etching polymers with ion beams: characteristics and results
451
Analytical forms (Yphysical): Thomson :
N2/ 3
Pul verisation level ~lhy.~i...· '" (atom/ion)
1
Us 1 + M2 cos O
:
-'. I
MI
I
cos 8
1
Y ex: - - ----=--:c-
"
(N : target atom ic den sity) Sigmund: Y(E, Us) ex: SN(E)/Us
1
Y(O)
Y(9) ex: - cos" 9
Anglen 50'
90'
Result ifMI t , Y t : if9t ,Y t: well verified when 9 < 60 0 •
3 Level of chemical pulverisation -
-
When using RIBE or IBAE, we can write: Ytotal = Yphysical + Ychemical If the projectile (P) forms with the target (T) a compound (TaPb) which is volatile, then in general, we observe that Ychemical S {; and the sign S takes into account the reflection of particles and the re-pul verisation of impl anted atoms ; If P and T form a non -volatile compound TaPb, we obser ve a decre ase in the velocity of attack on the target, so that Ychemical ;:: - (a~b) Y physical; When 0.25 < E < 2.5 keY, we tend to observe Yehemieal >- .JE; It has been observed that Ychemical ex: co s 9, so if 9 increases then Ychemical decreases.
II The relationship between etching speed and degree of pulverisation 1 At normal incidence
4
Surfa ce S
If N is the atomic den sity of the target and the volume eroded is equal to S x e (see Figure to left) then the number of atom s pulverised is N x S x e. During time At , the number of ion s incident to the surface S is equal to the flow of ions (D) multiplied by S. With D = J ~t in which q is the charge on mono. q charged IOns, NSe
Nq e
Nq
Y = - - = - - = - V. srt:.t/q 1 t:.t 1 With V = ~t we have the etching speed. In addition, it is po ssible to wr ite V = ~ Yl ex: Yl .
452 Optoelectronics of molecules and polymers
2 At oblique incidence The number of atoms pulverised is equal to N x S x e x cos 8. During time ~t, the number of ions incident to the surface at S is equal to D multiplied by S x cos 8. The result is again Y = !j9. ~t. By defining V(8)
ej
= -~t =
e· cos 8 ~t
,
we have:
,
Surface S
.
Y(8) = Nq V(8) J cos and we can also write: V(8)
1 = -Y(8)Jcos8 ex: YJ. Nq
Finally, we can always apply V ex: YJ when dealing with: -
non-reactive dry etching Y = Yphysical ; RIBE or IBAE in which Y = Ytotal = Y physical
+ Ychemical.
III Speed of reactive etching (IBAE Ar" /02 or 0+ /02) Degree of resurfacing (or fraction of absorbed surface): 8 = :;. , in which N is the surface concentration of absorbed molecule s and N* is the surface concentration of absorption centres. r is the flux of 0 2 and J is the flux of incident ions, so the flux of 0 particles absorbed is 2r1] (l 8) in which 1] is the probability of absorption for a molecule which hits an absorption centre . The degree of 0 atoms pulveri sed consists of 2 terms: •
•
0 atoms which have not reacted and is written a 8J, in which a is the level of pulverisation of 0 atoms which have not reacted and 8 the degree of absorbed surface; 0 atoms which have reacted and is written ~8J , in which ~ is the degree of reacted 0 atoms pulverised.
A-9 Etching polymers with ion beams: characteristics and results
453
At equilibrium, the number of absorbed 0 atoms equal s the number of pulverised o atoms and: 2fT] (1 - 8) - (ex . 8 . J + ~ . 8 . J) = 0, so
8=
ex
+~
(J) J« if
f , 8 = 1.
1+-- 2T] r
The etching speed is the sum of 2 components. One is physical and the other is chemical, each taking on the form Y x 1 in which J is the flux of incident ion s. For a unit surface (S = 1) of a given substrate, 8S = 8 take s on the chemical pul verisation while (l - 8)S = (l - 8) take s on the phy sical pulverisation. Thus:
IV ex Y chemical eJ + Y physical (l -
8)1
I
If the current of ions under study is 0+, we have to take into account the 0 + ions which attach themselves to the outer atom layers to yield reaction products. If y is the probability of an 0+ ion being fixed (implantation doe s not bring into playa 8-type coefficient for the absorbed surface), the contribution from the 0 + ion beam to the resurfacing of the target with oxygen is 2yJ.
The equilibrium equation becomes 2yJ + 2fT] ( I - 8) - (ex . 8 . 1 + ~ . 8 . J) With Q = rand
T]
= O.
<1> = ex + ~ , 2T]
we have J 1 +Q-
r 8=--7 J 1+<1>-
r
and retain:
IV ex Y chemical 8J + Y physical (l
- 8)1 I
If the reaction products are of the form XO n (in which, for polymers X is principally carbon), the probability of desorption being ~ (through pulverisation), and the number of 0 atoms which carry awa y X atom s is l/n, then the level of pulverisation of X atom s is: Y chemica l = ~ / n. From V we can deduce Ychemical, if Y physical is determined using an additional method, such as, for example, TRIM or empirically using a beam of Ar " ions .
454
Optoelectronics of molecules and polymers
IV Preliminary modelling of Yphysical for PI 2566 (a polyimide commecialised by Dupont and dedicated to microelectronics) For its use in microelectronics, PI2566 has a chemical formula which tends to favour etching, and can be used as an example to indicate typical etching parameters.
1 Levels of carbon pulverisation using 0+ ions Here the calculation is made on the basis of the surface bond strength (Us) being 7.4eV and with 2000 shots : • •
the chemical effects are not taken into account, so here are only cascading collisions or rather, physical effects; the level of pulverisation is at a maximum when E ~ 11 keV and e = 80° (Ymax ~ 1.36 atoms Cyion 0+). 1,4 ..---
-
-
-::::::;;;;;;r
-
-
-
-
--,
1.2 1
0.8
~:~ ~~~~~~~ 0.2 i
o
80 60
45 30
Incidence angle
e 15
'U
(0)
Ion energy (keV)
2 Comparing simulations of Yphysical (9) = f (9) and the Thompson and Sigmund models The various models show good agreement with TRIM obtained results. 45 , --
40
35
6'
30
-
-
•
TR IM (E
-
- - - - - - -- - - --
= 15 keY)
-
-
-
-
-
----,
- 0 - Thompson
Sigmund
>:'25 a> 20 >:' 15
......
10
5
o ~!=f:=-=:f=!!'==t=!=:t=!~~~~=-_+______l o 10 20 30 40 50 60 70 80 90 Angle of incidence
e (0)
A-9 Etching polymers with ion beams: characteristics and results 455
V Results from etching of polyimides 1 Self-supporting polyimide: the UPILEX Thi s material pre sent s high losses in opti cal absorption most likel y due to added pla stifying agents.
a Etching conditions The accelerating base energy was configured with the following optimised, and rather critical, parameters: (oxygen ions) E = 30keV,D = 10 17 ions cmI .J = 2I1-Acm- 2.
b Result A reasonably good result was obta ined in that an etching with depth 411-m was realised.
,
~
. . -
~ x 4 . 0 k 0012
10kV
leul
:--.l
c Nature of the etching With 0 + ions, there is no orientation effect from the beam (Sigmund or Thomson type laws are unverified for Yph ysical). With Ar" ions, and the same ion beam parameters, etching to 100 nm only is possible . If D ::: 10 17 ion s cm- 2, for 0+, the depth of the etching decreases a,d the polymer changes its appearance (due to a repeated depositing phenomenon).
456
Optoelectronics of molecules and polymers
d Conclusion Reactive etching due to oxygen chemi cal effects is extremely sensitive to the flow rate and can even greatl y influenc e the structure of the polymer, determining whether or not etching can take place. This test material , developed for its electrical properties, is not particularly well suited to optical applications, due to its high absorbenc y. With fluorinated polyimide s (for example Dupont's PI 2566), which are well suited to etching, more satisfying results were obtained (see Chapter XII, Section V).
2 A study of the etching of PI 2566 a Results from etching under accelerating conditions The parameters used come from those optimised for Upilex.
Nature of the ions 0+ was used with E = 30 keV, J = 211A em - 2, and the flow (D) was varied. In contrast to Upilex, the depth of the etching was insensitive (more or less constant) and remained relatively poor at e ~ 90 nm. Observation At D > 2 X 10 17 ionscm- 2 , the polyimide was degraded and could not be measured . Bubbles appeared due to strong local heating.
1400
~
1200
al 1000
..c B
"'" "'" "'"o"
is
•
800
•
•
•
600 400 200
0 0
5E+ 16
1E+17
1,5E+17
2E+ 17
2,5E+ 17
3E+17
Flow (ion crrr")
b Why? With 0+ ions, and also with Ar+ or He+ ions, a study of the effect of energy shows that e ~ Rp (see Figure below). In addition, under the ion beam the polyimide is very fragile and there is a formation , from the start of the irradiation (at E > 10 keV) of a hard layer with e ~ Rp (due to C = C and C = 0 bond ruptures and in consequence reticulation and contraction of the polyimide leading to e = Cte) which: -
limits (blocks) physical pulverisation (e ~ constant while D increa ses); and decrea ses the reactive polymer component in the polymer, which becomes just a thick carbonised layer.
A-9 Etching polymers with ion beams: characteristics and results
457
2500 . , - - - - - - - - - - - - - - - - - - - - - - - ,
•
Etched depth
2000
.g
.se,
.g 'E
]
1500 1000
500
0-+----+----+----+----+----+---+----1 10
20
30
40
50
60
70
80
Energy (keY)
c Conclusion These results indicate the import ance of keeping close to the RIE parameters (with an increase in J and a decrease in E which is of the order of only a few keV). Results obtained using parameter s close to the RIE are detailed in Chapter XII, Section V.
A-10 An aide-memoire on dielectrics: a model for double potential well and its application in determining the depth of trap levels
I Definitions of various dielectric permittivities [And 66] and the classification of different dielectric phenomena [Fre 60] 1 Absolute permittivity Generally, absolute permittivity (E) of an isotropic , dielectric material is defined as a quotient of an electrical induction formed by an electric field, so E= ~ . If we consider a charge (Q) caused by a potential difference (V) between the arms of a flat capacitor with surfaces S placed at a known distance (d) apart, the preceding ratio can be formed as: Cfreal Q/S Cd E= = = E V/ d S ' in which C is the capacitance. By consequence, in the meter, kilogram and second (MKS) system, the absolute permitti vity can be expressed in F m- I . If the system under study is a vacuum , then the vacuum permittivity (EO) is EO= 3Jn 10- 9 F m- I under MKS conditions, while in a centimeter, gram and second (cgs) system, EO= 1.
2 Relative permittivity It is often practical to introduce the term relative permittivity (s.) , which is also simply called, in an abuse of terms, permittivity . It is defined by the relation ship E= ErEOin which Er is a numbe r without dimen sion and equal in the ues system to absolute permittivity (or the dielectric constant), which explains the often encountered confusion between these two parameters. When an alternating tension (V = Voe j wt ) is applied to the flat condenser, which has a capacity Co when with an empty dielectric , the current which flows between the two plates on inserting a perfect dielectric (does not exhibit a leakage current) with permittivity Er can be written as
Q
1* = d . With dt
Q = CV = ErCOVod w t we have 1* = jWErCoV.
460
Optoelectronics of molecules and polymers
3 Complex relative permittivity As usual , in reality, the dielectrics in use are not perfect. They exhibit various sorts of currents, which we shall not detail for the moment, but give rise to a variety of similar effects. (Suffice to say that the effects of 'free' or 'bonded' carriers can give rise to heating effects or dielectric 'losses'). Such a current flow is entirely due to the dielectric material and we can characterise it with an imaginary component of the relative permittivity in the expression E; = E; - jE~ . In order to simplify the notation, the indices 'r' are often left out, and the reader is left to understand whether the system under study is working in relative or absolute permittivities. The intensity of the current thus becomes:
1* = WE~CO V + jWE;COV
= IR + jIe
I
The second term corresponds to a dephasing of between the tension and the purely capacitor based current. E; Characterises therefore the capacitor (insulator) part of the dielectric. The first term, relating to the fact that V and the intensity are in phase, corresponds to the resistive quality of the dielectric and is thus characterised by E~. The power dissipated by the Joule effect is thus written :
I
PJ = "2VoIo
I " 2 = "2COErWVo;
and the quantity E~ is called the dielectric absorption as it intervenes in the expression for the conversion of electrical energy to heat in the medium, thus absorbed by the dielectric and lost to the electrical circuit. liRI WE"CoV E" . = The quantity tan 1) = - .- = Ilel WE/CoV E/ is the (dielectric) loss tangent and allows a definition of the loss angle (1), which translates the dephasing between the resulting current and the 'ideal capacitor' part (Ie) of the current.
IR-~ The quantity Q = ~ s is a quality factor of the capacitor and is as large as tan 1) is small.
4 Limited permittivities Es is defined as the limiting (occasionally relative) permittivity obtained at low frequencies (the indice 'r' is removed by convention). At zero frequency we have a static field and Eoo is the (relative) limiting permittivity at very high frequencies (infinite frequency) .
A-1O An aide-memoire on dielectrics
461
5 Dielectric conductivity On taking the expressions E
= V/ d and Co = €oS/ d into 1*,
With 1 = aE and 1= ff 1 dS = IS , we can go on to the complex relation : 0'*
=
1 E =
1* " ES = W€o€r
+ JW€o€r . ,·
The real component for conductivity, called here the dielectric conductivity, is thus ad
= W€O€~ .
6 Classification of divers dielectric phenomena [Fre60] As already noted, the introduction of an imaginary term (10") into the dielectric permittivity, to take into account the existence of a current in phase with the applied tension , makes no presumptions about the origin of this current, whether how it is conducted or what losses may occur. In fact, there are numerous possible origin s of this dielectric absorption and we can class them, schematically, with respect to the frequency or temperature domain in which they appear : I absorption due to free carriers, for example , thermally generated carriers in the permitted band which exhibit a very low density ion insulators due to the limiting large forbidden band in these materials , or ions which permit ionic conduction at low frequencies; II the Maxwell-Wagner effect, due to charge accumulation in the discontinuities of the dielectric, found most notably in powders ; III the dipolar Debye absorption which is caused by bonded tied carriers and electrical dipoles; IV anomalies in 10' and 10" due to orientations of foreign molecules such as water at the solid surface; V anomalies in 10' and 10" tied with changes in phase ; and VI absorption due to resonance. Finally we present the Freymann representation [Fre 60] in Figure I below. Here the parameters of frequency and temperature are coupled. For a classical representation of 10' and 10" with respect to frequency only, we can turn to a textbook on electromagnetism, for example [May 96] or [Per 96]. Phenomenon I is due to a leak current resulting only from free charges, the number of which can be increased introducing impurities (such as ZnS, CdS doped with copper in analogy with semiconductors) into the dielectric. This results in an insertion of trap levels into the large forbidden band of the dielectric. Under a sufficiently high field, their electrons can attain a sufficiently high enough energy to collide with the lattice and provoke ionisations of the atoms . The upshot of this is that electrons are
462 Optoelectronics of molecules and polymers e
\A K 100Hz
1 MHz
e'
\:
A A\ 5
1Q MHz
V
~
High
temperatures
111
~
}j.
Low
temperatures
Figure 1. Representation of E' and E" as a function of l iT.
advantageously ejected into the conduction band to produce what is commonly known as a intrinsic breakdown of the dielectric. Phenomenon II is due to an accumulation of charges, such as electrons, in discontinuous regions within the dielectric. We can treat this problem as though studying a condenser made of several dielectric layers . Phenomenon III, otherwise known as a Debye dipolar absorption (DDA) generally results from the presence of neighbouring + and - charges (dipoles) which are linked so as to indisso luble, and act as pairs of tied carriers. The phenomenon is due to dielectric relaxat ions associated with the orientation of these dipoles once submitted to an electric field. The orientation occurs after a certain delay, characterised by a relaxation time . The dipoles exhibit a dephasing due to the inertia of their orientation with respect to viscous brushing against the rest of the material. We shall show in the following Section 2 how the hopping of a single charge over a potential barrier can be analysed following this sort of relaxation. Phenomenon IV can relate to a surface conductivity of the insulator, caused by 'semiconductors' such as dust, soilings and so on deposited on the insulator. This can also include surface humidity-impure water is a conductor with an extremely elevated dielectric constant of around 80. It is for this reason that the surface of a dielectric must be carefully cleaned prior to being studied . A usual methodology is to use alcohol first, to remove the humidity, and then a non-polar solvent such as benzene or toluene to remove the polar molecules, which could otherwise disturb the characterisation . And then of course , to work, if possible, in a dry atmosphere. Phenomenon V relates to an evolution in €' with changes in the dielectric density, caused by changes in phase , and above all, when the dielectric is a polar material, a degree of blocking of the dipoles in a new phase, for example when going from
A-1O An aide-memoire on dielectrics
463
the liquid to solid state. This mechanism can be accompanied by dipole 'frictions' between the dipoles and their environments giving rise to a heating effect in the dielectric which can be comparable to that due to a current. Phenomenon VI can be explained by considering that the charges of a dipole are elastically tied to an equilibrium position (in the simplest cases they can be compared to harmonic oscillators). Following the suppression of a field which displaced these dipoles from their equilibrium positions , they return to the equilibrium with a series of oscillations which display an amplitude which decreases as quickly as the breaking forces are strong. This model directly permits the possibility of an absorption due to resonance, which has a maximum at a characteristic alternating field frequency.
II Relaxation of a charge occupying two position separated by a potential barrier: dielectric model for double potential wells and its application to trap levels 1 Aide-memoire (see also Chapter IX, Section VII-2) The existence of trap levels in solids was demonstrated during the study of optical processes in semiconductors of groups II-VI. As an example we can take the spread of electronic levels in an inorganic phosphor such as ZnS(Cu), shown in Figure 2 and resembling that in Figure IX-14. Phosphorescence is due to a radiative emission which occurs with a delay after the initial luminous excitation, which excites electrons towards the conduction band (CB). The delay is caused by the passage of the same electrons, excited into the CB, through intermediates levels, called traps, in the forbidden band (FB). The relaxation from these traps is not instantaneous, thus the delay in the luminous emission and the persistence of phosphorescence, and occurs with a probability given by the Mott, Randall and Wilkins law, which states p = Vo exp( -U /k'I') , where vo is a constant for a group of traps . We can write t = l/p to detail the average trapping lifetime [Cur 60]. In contrast, fluorescence , caused by an instantaneous emission, results from an electron which does not pass through these intermediate trap levels.
CB
trapping detrapping (by thermal agitation of the crystal)
Trap U 2 FB
/v:-;;;;;
~hosPhorescence Figure 2.
464
Optoelectronics of molecules and polymers
Physically speaking we can characterise phosphorescence with respect to a thermal energy (kT)-loaned by phonons-which is involved in the transit of electrons trapped at an energy level A (the transition IA) towards another position with energyB by overcoming a potentialbarrierof heightV (the transitionlIB). The barrier corresponds to a trapping level E, with respect to the lowest part of the conduction band. Together, the transitions lA, lIB, and eventually, IIIp, make up the mechanism of phosphorescence. In addition, different trapping levels can exist, so we can have V, V2 and so on. 2 Transportation in a dielectric with trapping levels, and the effect of an electric field on transitions between trap levels a In the absence of an electric field
Here we shall look at an electron with two possible equilibriumpositions (A and B) separated by a distance a and a barrier V (assumed to be considerably greater than kT). The electron has as much chance of being found in A as in B, and the overall situation can be represented by a model of two potential wells separated by V, as in Figure 2-a. The probabilityper unit time for the electron to hop fromA to B (andreciprocally from B to A) is given by Poexp(- V /k'I'), where Po represents the same probability when the barrier is zero (i.e. when V = 0). At equilibrium, with N electrons per unit volume, all electrons of this type are equally spread between the two sites and the mean polarisation, due to these electrons, is zero. b When an electric field cib is applied in the sense AB (dielectrical measurements)
The potential energies VA and VB of an electron (of charge -q) differ by the quantity VA - VB = qaE. Given the orientation of the field, we have VA < VB, and by consequence(with V = -qV) VA is above VB by a quantity qaE, if the origin of the potential is taken as being at B (as in Figure 3-b). The symmetry of the system is thus broken, implicating a probability of presence of the electron being higher at B potential ener y
potential energy
distance
Figure 3.
A-lOAn aide-memoire on dielectrics
465
than at A, if we take into account the Boltzmann function which is proportional to exp (-U/kT).
c Expression for probability of transfer between wells Calculation of transition p robabilities Initiall y we assume that the electrons oscillate (with their therm al energy) about their equ ilibria positions with a frequency wo/2n . In the absence of a barrier, the probability that an electron will transfer from A to B or from B to A, in one seco nd, is thus wo/2n = Po. With a barrier of height (U - qaE ) on the A side and U on the B side, and in the presence of an electric field, these transition probabilities, respectively, PAB and PBA, become : Cl
PAB = _w_o exp ( __ u_-_q_a_E) 2n kT
(U)
PBA = -WQ exp - 2n kT
and
.
(1/)
If we suppose that qaE « kT, which typically is true for dielectric measurements taken under weak fields around I v cm'). we can go on to write: Wo UjkT (1 qa qa PAB=-e+E -) =PBA (1 +E -) . 2n kT kT
(I)
~ Variation in the number ofparticles in the A and B states at an instant t If at the instant t there are NA electrons in A and NB electrons in B, then there are NAPAB electron s which undergo the transition A ~ Band NBPBA elect rons which undergo the transition B ~ A, so that:
(2/)
On taking the difference between the above two equations and given that N = NA + NB is a co nstant and equal to the total number of electrons, then d (NB - NA) dt = -(PBA
+ PAB )(NB -
NA)
+ (PAB -
PBA)N .
(2)
On using eqn (I), PAB + PBA ~ 2PBA ( I
+ -qaE) 2kT
~
2PBA
(3)
and
qaE PAB - PBA ~ -PBA . kT Moving eqn s (3) and (4) into eqn (2) yields: d (NB - NA) qaE - - -- = -2PBA(NB - N A) + 2PBA- N. dt 2kT
The integration of this differenti al equation, without a seco nd member yields: NB - NA = C exp( - 2PBAt).
(4)
466
Optoelectronics of molecules and polymers
And moving this into the differential equation, while varying the constant C, gives: qaE
C = 2kTN exp(2PBAt) + K Byusingthelimitingconditionswhicharethatatt = O,NA = NB = N/2,determines that K = -i~N, from which can be derived that: NqaE NB - N A = - - ( 1 - exp[-2PBAt]). 2 kT
(5)
3 Expression for the polarisation at an instant t following the displacement of electrons a General case for displacement 8j in a system of qi charges at a concentration nj Moving the charge qi by Sj is the same as superimposing a dipole Slti = qiSj on the initial state . Schematically : OJ ~.
+ qj
.
by displacingq; by OJ
initial state
OJ ~
+qi
final state
To arrive at the final state from the initial, it suffices to superimpose on the latter a dipole Sltj = qjSj, as shown in the scheme below : s, iij ii;
• qi
~
+
•
~
-qj
0
I
+qj
011; =qi 0;
I
• 0
~
+qj
Similarly we can consider that the displacement of the charge qj by Sj is the same as applying a dipole Slti = qiSi . The polarisation (dipole moment per unit volume) associated with the displacement of charges qi by Sj is the same as applying a dipole moment per unit volume equal to Pi = niqiSj, where ni is the number of charges qi per unit volume . If there are other (i) types of charges (qj) present, then the polarisation is thus P
= LPi = LniqiSi . i
b Polarisation due to the displacement of N electrons-per unit volume-shared over a pair of wells with initial potential depth of U The two wells are separated by a distance a and, at an initial instant t = 0, are equivalent so that NA = NB = N /2 . Under the influence of a field E, the electronic charges
A -lOAn aide-memoire on dielectrics
467
(-q) are displaced by a distance +a for those in A and a distance -a for those in b, so: P
= Lniqioi = NA(-q)(+a) +
NB(-q)(-a)
i
(6)
= Ngqa - NAqa = qa(NB - NA)
Finally, on moving eqn (5) for (NB - NA) into (6) we acquire: N q2 a2 E P = 2kT(I - exp[-2PBAt]).
(7)
4 Practical determination of potential well depths a Basic formula Following on from eqn (7), if t -+
00,
P -+ Ps (static polarisation) we have:
N q2 a2E Ps = - - - . 2 kT
(7')
The term exp(-2PBAt) from eqn (7) describes the transitory regime of electrons trapped in potential wells and delayed (dephased) with respect to the applied field. As this varies exponentially with time, the relaxation of the system can be characterised by a macroscopic relaxation function: Y (t) = exp( - tiL) . The model for two potential wells thus can be seen in terms of a relaxation, much like that found in Debye 's theory, which yields similar equations for dielectrics (Debye's equations). The equivalence of the two terms obtained from the two well model and in Debye's theory (where Y(t) = exp( -tiL) as has been detailed elsewhere [leo 0I]), yields: exp(-2PBAt) = exp ( -~) ,
.
with L
I
= --. 2PBA
With PBA given by eqn (I ') , we can deduce: 11: L = _e U/ kT = Loe U/ kT WO
(8)
The term LO = 11:1Wo represents the duration of a single oscillation, as in the example A -+ B -+ A. In addition, as U » kT, we can find L » LO. The representation of the Debye curves shows us that E" goes through a maximum at a frequency Ve which is such that WeL = 1. Taking into account eqn (8) for L, we thus have: I 1 = 211:veLoeU/kT , so that Ve = -2-e- U/kT 11: LO In practical terms, the above formula is used in the form: Comment
U Log V e = - - - Log 211:Lo . kT
(9)
468
Optoelectronics of molecules and polymers
b Empirical characterisation Theoretically and as shown in Figure 4, we should obtain a straight line if we trace the logarithm of the critical frequency against inverse temperature. The slope of which should allow us to calculate the height of the potential barrier and the ordinance at the origin should yield the value of 1:0. In practical terms, we can arrive at the values for 1:0 and, above all, U, as we have done below with the example of Alq3. The law is in the form Vc = A exp(- U IkT), so that Log V c = - U IkT Log A. For I IT = 0, we have Log vc = Log A. The ordinance at the origin gives Log A, from which A = 1/2Jt1:0. In addition, when T = To we have Log vc = 0, so that liTo = k /U Log A which permits a calculation for U using U = kTo Log A. U is in eV with k = 8.64 x 10-5 eV K- I molecule",
+
Log v, Log A
Iff
Figure 4.
4 3.5
ech C6 Eact=O.217eV
•
3
............2
.-..
•
2.5 2
•
1.5
•
0.5
o 0.0035
0.0037
0.0039
0.0041
0.0043
1rr Figure S.
0.0045
0.0047
0.0049
A-IO An aide-memoire on dielectrics
469
c Experimental representation using Alq3 [Jeo Olb] The result of empirical observations is shown in Figure 5, from which U = 0.217 eV. This value is in good agreement with quantum chemistry calculations and thermoluminescence measurements.
A-II The principal small molecules and polymers used in organic optoelectronics
I Chemical groups and electron transport As indicated in Chapter X, a particular chemical gro up can be associated with a certain type of electron transport. As examples, the amine and carbazole functions favour p-type (hole) transport, while oxadiazole and triazole function s tend to favour n-type (electron) transport . Table I details their structures and characteristics. In general , metal based complexes act as electron s transporters.
II Examples of polymers used for their electroluminescence 1 The principal emitting polymers
Table 1. Functiona l group s and their favoured electrical transport Amine
Functiona l grou p
~/
I Conduction type Example
p TPD
Carbazole
Triazole
Oxadiazole
UD .cs. .cs. 0
~
I
I
p
n
n PBD
472
Optoelectronics of molecules and polymers
Table 2. The principal polymer based emitters (note abbreviations are widely used) Material
Amax (nm)
fluorinated polyquinoline (PQ) poly(para-phenylene) (PPP) polyalkylfluorene poly(3-cyclohexylthiophene) (peHT) poly(para-phenylene vinylene) (PPV) poly[2-methoxy,5-(2' -ethyl-hexoxy) - 1,4-phenylene vinylene) (MEH-PPV) poly(3-octylthiophene) (P30T) poly(3-alkylthiophene) (P3AT)
450 465 470 555 565 605 690 690
~)M n
(d)~" S
Figure 1. (a) PPP monomer unit (the polymer emits in the blue part of the visible spectrum); (b) PPV monomer unit (exhibits yellow emission); (c) MEH-PPV monomer units (emission is yellow-orange); and (d) P30T monomer unit (emits red light).
2 'The' polymer for hole injection layers(HIL)
n ~ n
Figure 2. The repeat unit of poly(3,4-ethylenedioxythiophene), which is often mixed with poly(styrene sulfonate), abbreviated commonly as PEDOT-PSS, to give an injection layer(HIL) .
A-II The principal small molecules and polymers used in organic optoelectronics
3 Example of a polymer used in hole transport layers (HTL)
Figure 3. The repeat unit of poly(N-vinyl carbazole) (PVK).
4 Example of a polymer used in electron transport layer (ETL)
Figure 4. Repeat unit of CN-PPV.
III Small molecules 1 The principal green light emitting ligands
JX)
0)
R = H : 8-hydroxyquinoline (q) R = CH 3 : 2-methyl-8-hydroxyquinoiine (mq)
7-azaindole
~
R
~
N
~
#
OH
N H
lO-hydroxybenzo[h]quinoline (Bq)
Figure 5. The structure of the principal ligands.
N
473
474
Optoelectronicsof molecules and polymers
2 Principal electron transporting small molecules emitting green light
Figure 6. Structures of the molecules: beryllium bis(lO-hydroxybenzo(h)quinolinate) (Bebqj) ( Aphotoluminescence = 529 nm); magnesium bis(2-methyl-8-hydroxyquinolinate) (Mgmqj) ( Aphotolumin escence = 487 nm); and aluminium tris(8-hydroxyquinolinate) (Alq3) ( Aphotoluminescence = 504 nm).
3 Example electron transporting small molecules emitting blue light
Zn (bis salen-t), Q-o-zn_o-y CH==N-1CH,~N==CH
Q-o--~-~ CH=N f cH , t N=HC
Zn (his salen-n),
Figure 7. Structures of Zn (bis salen-njj and the particular case of zinc bis(2-hydroxylatebenzylideneamino) butane (Zn (bis salen-4h,) which displays Aphotoluminescence = 460 nm.
4 Example small molecules which emit red light Small molecules which emit red light are principally based on europium octahedral complexes in which ligands (L) derived from ~-dicetone or aminopyrazine saturate the co-ordination sphere of the lanthanide (M) along with phenanthroline,
A-II The principal small molecules and polymers used in organic optoelectronics
475
or two electron donating molecules such as triphenylphosphine oxide or dibenzyl sulfoxyde.
5 Examples of small molecules whichserve principally as hole injection layers (HIL)
Figure8. Structure of copper phtalocyan ine (CuPc).
6 Examples of small molecules servingprincipally in hole transport layers (HTL)
Figure 9. Structures of the molecules : N, N'-diphenyl-N, N'-(3-methylphenyl)-I , l '-biphenyl4,4'-diaminc (TPD); 4,4-bis[N -(l-naphthyl)-N-phenylamino]biphenyl (NPB) ; and 4,4' ,4/1tris[N -( l-naphthyl)-N-phenylamino]triphenylamine (TNATA).
476
Optoelectronics of molecules and polymers
7 Example of a small molecule servingprincipally to confine holes in 'hole blocking layers' (HBL)
Figure 10. Structure of bathocupuroine (BCP).
A-12 Mechanical generation of the second harmonic and the Pockels effect
I Mechanical generation of the second harmonic (in I-dimension) 1 Preliminary remark: the effect of an intense optical field (E W ) Non-linear effects occur when the force (with E = E W ) returnin g displaced electrons towards their equilibrium position is no longer of the form fr = -kx = -mw2x. It is the Coulombic force developed by nuclei, which is exerted between nuclei and electrons, that gives this returning force . Typicall y, these internal electric fields are of the order of 108 to 109 V em -1 , while the optical field developed from several MW em - 2 is only of the order of 104 V em - 1. When the optical field is no longer negligible with respect to the internal field, for example on the use of a laser, the returning force must be rewritten in the form fr = -kx + dx 2 = -mw2x + m&2x, and is thus privileged by an inharmonic potential (W, although commonly denoted by V): ~
~
F = -grad W = -grad V
===}
I 2 I 3 V = -kx - -dx .
2
3
2 Placing the problem into equations The inharmonic potential , which takes on the form V (x) = ~ kx 2 - tdx3, along with the corresponding returning force fr = -kx + dx 2 are schematised in Figure I. The response of the system, in terms of displacements, due to an optical excitation (electrical field E W = Eo cos cot) is governed by the fundamental dynamic law for which a displacement x(t) is formulated with respect to the various harmonic components.
478
Optoelectronics of molecules and polymers 1
1 2
(a)
1
Vex) = - Ja2 - - dx 2 3
Vex) =-Ja2
3
(b)
l[~
i, (x) = -h+dx2 = -maJo x +m02;;2
i, (;;) =-h
Figure 1. Representation s of: (a) harmonic potentials; and (b) inharmonic potentials, each shown with their corresponding forces.
With the system being non-linear, we have to be prudent in using our habitual imaginary notation (E W = Re (Eoe j wt )) , and have to work alway s with real functions. On denoting the conjugated complex by cc, we have
EW
= E cos cot = ~ (e j wt + cc) .
When we study the movement of electrons in a material using classical forms (in the linear regime with a returning force fr = -kx), we ~an bri~~ in all the applied force s in the system, which include the Coulombic force fc = qE , in which q is the charge under study (q = -e for electrons), the friction force (ft ) , which is such that f t = -mfv x = -mfx,andthereturningforcefr = -kx (see, for example, Chapter 4 of [May 96]) . The same route can be used in non-linear regimes, although we must take on board the new expression for fr , as in fr = -kx + dx 2 = -mw2x +
mS2x. The fundamental equation for the dynamics with respect to x can thus be written as: mx = F = fr + ft + fe, so as to give, on simplifying withm:
L
(1)
A-12 Mechanical generation of the second harmonic and the Pockels effect V(r)
(a)
479
= ~/ci'- - ~dx 3 2
3
(b)
I
second harmonic _ _-t-l_ _-+_ X
1
-I--~---,-r---+-~--_
P
-
Dec omposition
/
tim
Movementdue to
fundamental mode
continuous mode
E(t) = E cos <:ot
Figure 2. Displacement of a charge placed in an inharmonic potential (a) and its decomposition(b).
Under a permanent regime, x is thu s sort after in a form which displays its development with respect to the harmonic components:
x(t) =
~ (xo +
x le iwt + x2ei2wt + .. . + cc) .
(2)
To simplify the calculation we can take Xo = a (even if the term exists: see Chapter XII, Sect ion III , studies therein) . The resolution of the problem is sadly through long, laborious calcul ations , which involve inserting eqn (2) for x(t) into eqn (I) . The result is the startlingly long equation (3) :
_
~2 (XIeiwt + cc) _ 2
200
2
(x 2e 2
iwt
+ cc) +
i~r (XIeiwt + cc) + ioor(X2eiwt + cc) 2
i2wt + 002° ( Xl e + cc ) + 002° ( X2 eiwt + cc) + 002° ( x2ei2wt + cc ) -
~
(xie2iwt +2xlx2'e- iwt +xlx7 +X2X2' +2x lx 2e3iwt
qE ( 1.wt ) = 2m e +cc
+x~e4iwt +cc) (3)
480
Optoelectronics of molecules and polymers
3 Solving the problem
a First order terms (linear approximation) Identifying the coefficient to the e iwt terms in eqn (3) gives X]
qE =-
I
m (w6 - (
2)
qE
+ iwf
I
~ ---------
2wm (wo - co) + i(fj2)
(4)
t if resonating at wo = co The linear polarisation for a displacement xr (t) of the charge q is thus p(l) (t)
= Nqxj (t) = Nq ~l
(e iwt
+ cc) .
By identifying with
we obtain (w)
Xl
Nq
I
= mEo (w6 -
(
2)
+ iwf
(5)
(here of course we find again the expression for the dielectric susceptibility of a linear medium; see eqns (4-36) in [May 96]) .
b Second order terms In the same way as for the linear system, the identification of the coefficients for e i2wt allows us to determine X2, which is such that
xf
(term dx 2 in the relation fr = -mw6x + We can thus see that it is the term in m82x2 = -kx + dx 2 ) which generates (forces) the movement in 2w. On moving eqn (4) for Xl into our latter equation, we arrive at:
The second order susceptibility appears within the second order term of the polarisation, which is written by analogy to the linear polarisation as
A-12 Mechanical generation of the second harmonic and the Pockels effect
481
From which we can thereforededuce X~2w) : (2w)
X2
Nq3 S2
I
= 2m2Eo [( w5 _ ( 2 ) + iWf]2 [( w5 - 4( 2 ) + 2iwf] .
(7)
xi
In a similar manner to X~w), 2w ) presents both real and imaginary parts but does, however, have a denominator which exhibits double resonance, as in co = wo and ~ w=2' Comment J Here the charge under considerationis that of an electron, i.e. q and thus q3 = _e 3. We can thus rewrite eqn (7): (2w)
X2
=-
Ne3 S2 2m2EO
I
[(W5 - ( 2 ) + iWf]2 [(w5 -
4( 2 )
+ 2iwf]'
= -e, (7/)
Comment 2 In addition, we can establish the following relationshipbetween linear and non-linear susceptibilities, respectively, X~w) and 2w ) :
xi
~2
(2w)
X2 (W)]2
.[ Xl
(2w)
Xl
2 EO
= ~ = 1;(2w) 2N2q3
The parameter 1; (2w) , called Miller's paramter, is in fact practically identical for all materials: 1;(2w) ~ 3 to 8 X 109 SI for InAs, GaSb, GaAs, Cd'Ie, ZnTe and ZnSe. Comment 3 In this Section we have looked at the problem in one dimension only. If instead of consideringan incident wavewith only one component, we imaginethat it presents three components, then the second order polarisation will have components Px , Py and Pz , which generallycan be obtained by using all possible quadratic components of Ex, Ey and Ez, as in:
Ex2 EY2 E2z , in which X~(2w) is thus a tensor. EzE y EzE x ExE y
II Excitation using two pulses and the Pockels effect 1 Excitation from two pulses
While studying the mechanical generation of the second harmonic, we have shown, in a classicalmanner, that an excitationdue to a photon (E W ) can generate movements
482
Optoelectronics of molecules and polymers
with frequencies of co (movement Xl(tl) and of 2w (movement X2(t». Respectively, photon emissions from charges which move through XI (at a frequency co) and through X2 (at a frequency 2w) do so by emitting dipolar rays at the frequencies wand 2w. We can thus generalise this emission mechanism for an excitation in a system of two photons with pulsations w' and « " , We should allow for the emission detailed the Figure 3: For a system excited with a pulsation co, we can use the classic eqn (7) for the second order (relative) susceptibility as follows: for an excitation pulse at Wi, given D(Wi) =
w6 - wf + iWir, eqn (7) becomes: (8)
and , similarly, for a two wave excitation pulsating at w' and «", the pulsation harmonic (WT = w' + co") is associated with a second order susceptibility in the form:
= Nq302
(w'+w")
'1...2
I
2m2co D(w/)D(wl!)D(w'
+ wI!)
(9)
2 The Pockels Effect A particular case which draws interest is when there is an incident optical wave (with pulsation w' = co) and a second wave at low frequency. At the limit zero, for a static field (wI! = 0), the preceding eqn (9) becomes:
X
(w+o)
2
Nq 3 02 I --- 2m2co D(O)D(w)D(w)
(10)
This second order susceptibility depends only on the optical pulsation co. Nevertheless, a reduction to the single, varying polarisation term is inexact, as we shall see . If we write the expression for the polarisation using the more usual development (see Chapter XII, Section III-2) , we have pet) = Po + XalE(t) + Xa2E2(t) + ... , in which here E(t) E(o) + E(w)ejwt + cc and where Xa is the absolute susceptibility, we can see that the dependence of the susceptibilities with two pulses
=
(J/:J
I~:~
------' to"
- -•• 2m'
:::---. zo"
~
( ' + q mH) In . W hiICh P and q are Integers " pm
Figure 3. Possibleemissions from a system excited by pulses at 00' and wI!
A-12 Mechanical generationof the second harmonic and thePockels effect
483
(static and optical) involves some complications in the calculation. In fact, we end up writing that (with relative susceptibilities to the 1st and 2nd order of Xl and X2) pet)
r
= £0 {Xl [E(O) + E(w)e jwt + cc] + X2 [E (O) + E(w)ejwt + cc + ...}
(11)
We can quickly see that this description is completely ambiguous as, for example, the first term (XI) carriers both the static term (E(o) and the optical term (E(w)e jwt) . If we continue with the calculation, even given the previous remarks (and thus Xl = XI(0) w or XI = XI (co) == ) by notation) while limiting ourselves to the static term and the pulsation term co, we have:
xi
pet) = £O{[XI(O)E(o) + Xl(w)E(w)e
jwt]
+ [X2(0)E{0) + 2X2(0 + co)
x E(o)E(w)e jwt]} + ... = {£o [XI(0) + X2(O)E(o) ]E(oJl
+ {£O[X I(co) + 2X2(0 + w)E(o) ]
x E(w)e jwt} + .." which gives a polarisation of the form: pet) = Po + Po+w(t)·
(12)
We can see here that the polarisation varying in co (the term Po+w(t» depends on + co) and also on XI (co) . A polarisation with frequency co is thus in the presence ofE(o), so: jwt Po+w(t) = £0 [Xl (co) + 2X2(0 + w)E(O) ] E(w)e . (13)
W2 (0
The indice 0 + co for Po+w(t) indicates that the polarisation is independent of co in the presence of the static wave E(o) and the optical wave E(w). This polarisation is a linear function of E(w)e jwt although it is calculated in the presence of the static field E(o). Additionally, in the absence of the static field E(o), we have as polarisation due to the pulse co, Pw(t) = £O(£r(w) - I)E(w)e jwt. With (£r(w) - 1) = Xl (co) = n2 - I, in which n = n(E(o) = 0) = n., using the notations detailed in Chapter XII (Section IV-5) we can write Pw(t) = £0(n2 - I)E (w)e jwt = Xl(w)E(w)e jwt. If we now consider the expression which takes on this polarisation in the presence of a static field E(o), this supplementary polarisation changes the indice to the form n + ~n, and we find that pet) = £o [(n + ~n) 2 - 1][E(o) + E(w)e jwt]
= £o[(n + ~n) 2 - I]E (o) + £o [(n + ~n) 2 - I]E(w)e jwt = Po + Po+w(t)
so that:
Po+w(t) = £o[(n + ~n)2 - l]E (w)e jwt .
By identification of Po+w(t) in eqns (13) and (14), we obtain:
(14)
484
Optoelectronics of moleculesand polymers
[en + fj,n)2 - I] = [Xl (00) + 2X2(0 + w)E(o)], so that with XI (00) = n 2 - I and [en + fj,n)2 - I] ~ n 2 + 2nfj,n - 1. This gives us 2nfj,n = 2X2(0 + w)E(o). And this we arrive at the definitive equation A
zxn =
X2(0+W)E (0). n
(15)
The variations in the indice appear to be proportional to the applied field E(o). However, this qualitatively exact result for the dependence of fj,n on E(o) is very imprecise with respect to the function in n due to the presence of the term X2(00 + 0), itself coming from the rather ambiguous eqn (11). A more phenomenological and alternative method, which takes account of the dependence of the optical indice on the static polarisation field-in organic media-is proposed in Chapter XII, Section 5. We can though go on to exploit eqn (11) by remarking that from eqn (5):
N
XI(W)
I
q =-mEo D(co) 2
and that D(O) = 005 = Cte, and from which, after eqn (11), (w+O)
X2
2 2 N q 2~2 o m EO 2 = -2 2 -N 4 XI(w) 2 m EO q 00 0
' - v - " '-v-'
I
I
D(w)D w
D(O)
(which resembles Miller's relationship) &2100
= 2 2N 2 XT(w), 00 0 q If with XT(w) = (lOr - 1)2 = (n 2 - 1)2 ~ n4 (and assuming 1 to be negligible with w O respect to n 2), we have + ) ex n4 •
xi
If we move this law into eqn (15), we find:
n4
fj,n ex - E(o), n that is fj,n
I 3 = "lrn s,
where E(o) = Es, and r is a coefficient of proportionality.
Comment It is worth noting that X(2w) comes from the term of xT (resulting from the term for dx 2 from the inharmonic force f = -kx + dx 2) so as to relate to the pulsation 200 . w O + ) corresponds to a pulsation of co. We have shown in Chapter XII, Section IV, that we do not have to return explicitly to the inharmonic term, thus simplifying greatly our calculations.
xi
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Index
absorption (spectral), 184,401 acceptor-donor, 195, 326 adjusting emissions, 285 ageing, 294 aggregates, 194 Alq3, 61, 69, 94, 259 amorphous silicon xi Anderson localisation, 47 anodes (OLEDs) 278 anthracene (narrow band) , 109 band curves, 261 forbidden, 6 HOMO, 65, 75 Hubbart's, 43 LUMO, 65, 75 scheme, 92, 96 structures, 33 barrier - at inte rfaces, 259 benzene (electron structure), 66 bilayer heterostructure, 324 OLED,280 photovoltaic cell , 322 bipolaron, 82, 86 Bloch (function), 395 Boltzmann (transport equation), 404 bond strong, 4, 9 weak , 3, 6 cathodes (OLEDs), 278 cathode-virtual, 139 cha in
of atoms , 12,26,389 distorted, 20 characteristic s I(V), 264, 271 charge transfer complex, 45 chromophore, 177 coefficient s - opto-electric, 341, 356 conduction-organic (n- or p-type), 276 conductivity, 99 conduction by hopping, 112 configuration curves, 87, 168 diagram of, 179 electron, 164, 443 conjugation (molecule/polymer), 62 contact at electrodes, 259 , 268 ohmic, 138 rectifying , 135 coupling between atoms, 39 between molecul ar orbit als , 40 electron-lattice, 77 Frank-Condon, 184,264 current bipolar, 157 equilibria, 277 saturation, with traps, 147 space cha rge limited, 139 volume controlled, 154 Davidov (displacement, breakdown), 192 defaults (effect s of), 90-93 depo sition, 201 assisted, 204 vapour phase, 202
496
Index
Dexter transfer, 197, 288 dimer,189 diodes inorganic, 236 molecular optic, 349 organic, 253, 257 white, 296 donor-acceptor, 346 dopants electrical, 126 optical , 286 doping, 87, 126, 431 Dushman-Richardson law, 136, 433 electric (transport properties), 99, 133 effective mass, 35, 396 electro-optic modulator, 358, 368 electron pumping, 292 emission electrical (laws), 135 optical internal/external, 221 encapsulation, 203 etching, 216, 449 ofITO,211 of pixels, 298 RIBE /IBAE, 366 speed, 451-452 excitation transfer, 286 exciton, 87, 185 charge transfer, 186 dissociation, 322 Frenkel, 188 Wannier, 186 fabrication (techniques), 201 fill factor, 318, 333 film, 204 film growth , 205 Floquet (theorem), 9 fluorescence, 182, 194-195 flux, 406 Forster (transfer) , 196, 289 Fowler-Nordheim (emission), 137,437 fullerenes, 61, 70, 397 gauss (trap distribution), 154 Graetzel cells , 320 guides diffusion , 232 fabrication, 213 losses, 233, 368
half-wave tension, 344 heterojunction OLEOs, 253 volume , 325 hopping nearest neighbour, 112 over variable distance, 113 polarons, 116 Hubbard (band), 43 hybridisation, 36, 381 hopping (see conduction by hopping) improving OLEOs, 274 infra-red OLEO s, 291 injection (level of) , 133 ink-jet, 305 ink-jet technology, 302 interaction dipolar, 196 intrachain, 66 interchain, 67 Ioffe-Regel, 48, 51 irradiation, 94 Jablonsky, 181-183 Kaiser's model , 129 Kerr effect, 341 Kubo-Greenwood, 403 laser (effect) , 292 layer confinement, 279, 476 emitting, 284,474 injection, 280,473,474 transport, 282, 473, 474 layering , 279 light amplifier, 173 limits conduction model with delocalised states band , 105-109 rigid band theory, 48 liquid crystal, 239 localisation (Anderson), 50 luminance, 220 measuring, 230 luminescence extinction, 248 Mach-Zehnder, 364 matrix active, 243 doped, 165 passive, 243
Index merit factor, 359 merit figure, 360 microcavities, 292 Miller and Abrahams, 52 mobility, 51, 101, 107-108,412---413 in Alq3 265-266 in polymers, 271 thermally activated, 421 molecule centrosymmetric, 349 non-centrosymmetric, 350 Mott (localised states), 54 Mott and Gurney (law), 140 MIM structure (metal-insulator-metal), 321 MIS structure (metal-insulatorsemiconductor), 252 multi-layers - see layering OLEDs, 253, 257 optical losses, 233, 368 orbitals - atomic and molecular, 373 page - flexible electronic, 304 Peirls (transition), 24, 64 permittivity - dielectric, 459 phases - interpenetrated, 324 photodiode (sensitivity), 226 photovoltaic, 195, 313 phosphors, 249 phosphorescence 182, 250 photoluminescence, 184 photometry (scaling) , 217 phtalocyanines, 316 pixels, 298 Pockels effect, 343 polaron, 77, 86 polaron - exciton, 88 polaron - transverse , 126 polyacetylene, 64 polyimide, 363 polymer degenerate -(CH)x-, 64 non-degenerate (PPP), 65 polymerisation in the vapour phase (VDP), 203 poly(para-phenylene) (PPP), 60, 65, 86, 94 poly(phenylene vinylene) (PPV), 60, 184 Poole-Frenkel (conduction), 159 pulverisation time, 449
quantum interferences, 104 rare earths , 164, 169-173 relaxation, 409 energy, 25 time, 417 rules circumnavigating (bending), 288 transition , 163, 176, 180,444,447 Schottky emission, 136, 434 screen electroluminescent, 246 liquid crystal (LCD), 239 micro-points, 245 organic, 296 plasma, 244 soliton, 88 state antibonding, 30, 379 bonding, 30, 379 densities, 22, 406 localised , 41, 50-56 substrates (preparation), 211 system degenerate, 103 host-guest, 362 non-degenerate, 105 thermoelectric power, 423 transition metal-insulator (Peierls), 24 metal-insulator (Anderson), 54 Mott-Hubbart, 44---46 permitted optical , 180 transition metals, 166, 171, 177 transport electron, 74, 99 polarons , 116 transport mechanisms, 99, 127, 133 traps, 144, 264, 463 distribution, 151 yield energetic, 274 external quantum , 221, 273 fluorescence quantum, 274 internal quantum, 221, 273 measure of, 226 photovoltaic, 333
497
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